N769AS

Part: SKIN — CRACKED (BS 447-448) · airframe 72,584 hrs · 41,798 cycles

FUSELAGE SKIN HAS A CRACK AT CHEM MILL STEP STR 1, BS 447 - 448.5. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN ON T/C AD20121204-400-53-3.

Part: SKIN — CRACKED (BS 437-439) · airframe 72,584 hrs · 41,798 cycles

FUSELAGE SKIN HAS A CRACK AT CHEM MILL STEP STRINGER 1 BS 437 - 439. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN ON T/C AD20121204-420-53-3.

Part: FRAME — CRACKED (BS 500D) · airframe 72,584 hrs · 41,798 cycles

1.04 WIRE PENETRATION HOLE ON FRAME CRACKED AT BS 500D ON AFT SIDE BETWEEN STRINGERS 20 AND 21L. ACFT GROUNDED. REPAIRED THE FRAME IAW SRM 53-00-07-2R-20.

Part: STRINGER CLIP — CRACKED (BS 500C) · airframe 72,584 hrs · 41,798 cycles

FWD CARGO BAY BS 500C STRINGER CLIP AT 22R IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0.

Part: BEAR STRAP — CORRODED (BS 490) · corrosion level 2 · airframe 72,584 hrs · 41,798 cycles

FWD CARGO DOOR CUTOUT AFT SIDE INTERNAL BEARSTRAP HAS CORROSION UNDER SFT CORNER SCUFF PLATE LOCATION. ACFT GROUNDED. REPAIRED THE BEARSTRAP IAW EA 400-53EA-18213 REV 00.

Part: BEAR STRAP — CRACKED (BS 344) · airframe 72,584 hrs · 41,798 cycles

FWD ENTRY DOOR CUT OUT LOWER AFT CORNER HAS A CRACK ON BEAR STRAP. GROUNDED - YES. REPAIRED DAMAGE TO SKIN IAW B737 400 SRM 53 10 01 2R 12. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 60,000 TOTAL FLIGHT CYCLES OR 12,000 FLT. CYCLES AFTER REPAIR INSTALLATION, WHICHEVER COMES LATER. REFER TO OPERATORS REPAIR ASSESSMENT GUIDLINES FOR METHODS AND INTERVALS.

Part: ROLLER — OUT OF POSITION (L2 WINDOW) · airframe 72,259 hrs · 41,577 cycles

CAPTAIN'S SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. ACFT GROUNDED. FOUND AFT LOWER ROLLER CAME OFF FROM AFT LOWER BELLCRANK, REF AMM 56-12-11-825-001. REPLACED LOWER AFT ROLLER & SHIMMED. ALSO UPPER ROLLER SHIMMED FOR PROPER ENGAGEMENT IAW AMM 56-12-11-404 & 56-12-11-825-001. WINDOW HEAT TEST ACCOMPLISHED, REF AMM 30-41-00-735-047. VERIFIED HANDLE FORCES WITHIN LIMITS. WINDOW TRACKS LUBED. ALL OPS CHECK GOOD. OK FOR SERVICE.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 71,808 hrs · 41,244 cycles

F/A REPORTS L-1 DOOR HARD TO CLOSE. ACFT GROUNDED. FOUND L-1 DOOR NOT COMING IN PARALLEL WITH DOOR CUTOUT. ADJUSTED L-1 DOOR GUIDE ARM REF AMM 52-11-21. L-1 DOOR OPERATES NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 71,212 hrs · 40,855 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT RT AFT OVERWING EXIT IS MISSING LENS. ACFT GROUNDED. REPLACED LENS AND TESTED LIGHT ASSY IAW AMM 33-51-81-962-011. OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,427 hrs · 40,353 cycles

EXIT SIGN, ROW 17, ACFT RT IS MISSING. ACFT GROUNDED. REINSTALLED LENS COVER AT 17F, OK FOR CONTINUED SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,095 hrs · 40,122 cycles

CURTAIN DIVIDER FWD EMERGENCY EXIT LIGHT LENS CONER BROKEN. ACFT GROUNDED. REINSTALLED EXIT LIGHT LENS AT CLASS DIVIDER, REF MM 33-51-11.

Part: INTERCOSTAL — CRACKED (BS 767-787) · airframe 69,915 hrs · 40,014 cycles

INTERCOSTAL BS 767 TO 787, STR 27R IN CRACKED AT FASTENER HOLE. FOUND UPON REMOVAL FOR BS FRAME REPLACEMENT. ACFT GROUNDED. FABRICATED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0 AND RESTORED FINISH IAW SOPM 20-41-02.

Part: INTERCOSTAL — CRACKED (BS 787-807) · airframe 69,915 hrs · 40,014 cycles

AFT CARGO INTERCOSTAL BS 787 TO 807, STR 24L IS CRACKED ON UPPER FLANGE UNDER NET TIE DOWN PLATE, FOUND UPON REMOVAL FOR BS 807 FRAME REPAIR. ACFT GROUNDED. FABRICATED NEW INTERCOSTAL, BS 787-807 AT STR 24L IAW SRM 51-30-01-OG-0 TO BE INSTALLED ON MIG 5, SN OK 5143.

Part: CHANNEL — CRACKED (BS 500-500A) · airframe 69,915 hrs · 40,014 cycles

IN FORWARD CARGO BILGE, AFT OF CARGO DOOR. SUPPORT STRUCTURE, PAN, AROUND VHF COM ANTENNA IS CRACKED IN SEVERAL PLACES. ACFT GROUNDED. R & R NR 1 VHF SUPPORT CHANNEL IAW SRM 51-40-02-0G-0.

Part: DOOR SILL — CORRODED (BS 787-847) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

WHILE ACCESSING FOR BS 794, FRAME REMOVAL FOUND AFT PIT CUTOUT LOWER BEAM SILL UPPER STRAP HAS CORROSION ON LOWER SIDE. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, LOCATED AND DRILLED NEW UPPER STRAP IAW SRM 51-40-05-0G-0 TO BE INSTALLED ON MIG 5, OK 5590, W 1.5, O .100, R .082, L 10, D .018.

Part: FRAME — CORRODED (BS 794) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

AFT CARGO FRAME BS 794, STR 25R CORRODED, FOUND AFTER REMOVAL OF INTERCOSTAL FOR ACCESS TO 787 FRAME EXISITNG REPAIR. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. R & R BS 794 FRAME IAW SRM 51-40-02-0G-0, W 2", O .071", R .063", L 6", D .008".

Part: ANGLE — CORRODED (BS 500G) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

FLOOR ANGLE AT BS 500G IS EXFOLIATED STR 25L TO STR 25R. ACFT GROUNDED. REMOVED DAMAGED ANGLE , FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0.

Part: ATTACH FITTING — CORRODED (BS 992) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

BS 992, STUB FRAME LT SIDE LOWER END ATTACH CLIP CORRODED. ACFT GROUNDED. R & R LT 992 STABILIZER FRAME LOWER ATTACH CLIP IAW SRM 51-40-02-0G-0, W 1.2, O .094, R .000, L .5, D .094.

Part: DOUBLER — CORRODED (BS 947-952) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

INTERCOSTAL DOUBLER, STR 21R, BS 947-952 IS CORRODED. ACFT GROUNDED. R & R INTERCOSTAL DOUBLER BS 947-952, STR 21R IAW SRM 51-40-02-0G-0, W 3.0, O .032, R .022, L 2, D .010.

Part: FLOORBEAM — CORRODED (BS 500G) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

FLOOR LT ANGLE AT FS 500G IS EXFOLIATED STR 25L TO STR 25 R. ACFT GROUNDED. REMOVED DAMAGED LT ANGLE , FABRICATED NEW LT ANGLE AND INSTALLED NEW LT ANGLE IAW SRM 51-40-02-0,G-0, SRM 51-40-05-0.

Part: INTERCOSTAL — CORRODED (BS 927-947) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

LOWER END OF 947 STUB FRAME AT 21R INTERCOSTAL HAS AREAS OF CORROSION. ACFT GROUNDED. CORROSION FOUND OUT OF LIMITS, R & R INTERCOSTAL IAW SRM 51-40-02-0G-0, W 3, O .032, R .025, L 5, D .007.

Part: SUPPORT ANGLE — CRACKED (BS 270-291) · airframe 69,915 hrs · 40,014 cycles

FWD ENTRY WAY UPPER LOBE FWD OF R1 DOOR AT BS 270 - 291 HAS CRACKED IN INTERCOSTAL SUPPORT ANGLE FWD OF R1 DOOR CRACK LOCATED BELOW STRINGER 9. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CRACKED (BS 270-291) · airframe 69,915 hrs · 40,014 cycles

FWD ENTRYWAY UPPER LOBE FWD OF R1 DOOR AT FS 270 TO 291 HAS CRACKED INTERCOSTAL SUPPORT ANGLE BELOW STR 9. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 520-540) · airframe 69,915 hrs · 40,014 cycles

LOWER FUSELAGE GROUND AIR CONDITIONED SERVICE DOOR LANDING IS DAMAGED. ACFT GROUNDED. UPON FURTHER EVALUATION, FOUND GROUND AIR DOOR LANDING CRACKED. REPAIRED AT GROUND AIR CONDITIONED SERVICE DOOR LANDING IAW SRM 53-30-01-2R-2, REPAIR 2. THIS IS A CAT B REPAIR WITH INSP THRESHOLD OF 30,000 FLIGHT CYC AND A REPEAT INSP INTERVAL OF 30,000 FLIGHT CYC, CURRENT FLIGHT, CYC 40,014.

Part: CREASE BEAM — CORRODED (BS 767-787) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

RIGHT CREASE BEAM WEB IS CORRODED BS 767-787. ACFT GROUNDED. R & R RT CREASE BEAM IAW SRM 51-40-02-0G-0, W 4, O .032, R .012, L 2.75, D .020.

Part: CREASE BEAM — CORRODED (BS 492-500) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

RT CREASE BEAM WEB IS CORRODED BS 496. ACFT GROUNDED. REMOVED CORROSION ON CREASE BEAM WEB BS 496-500 IAW SRM 51-10-02, W 2.50", O .036, R .023, L 3.70, D .013, MATERIAL LOSS OUT OF LIMITS IAW SRM 53-31-13, DETAIL II. NEW WEB FABRICATED ON MIG 5 OK 5289. R & R WEB IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 727C-727D) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

RIGHT CREASE BEAM WEB IS CORRODED, BS 727C-727D. ACFT GROUNDED. R & R RT CREASE BEAM WEB BS 727C -BS 727D IAW SRM 51-40-02-0G-0, W .5, O .032, R .019, L 3.0, D .013.

Part: CREASE BEAM — CORRODED (BS 727E-727F) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

RIGHT CREASE BEAM WEB IS CORRODED, BS 727E-727F. ACFT GROUNDED. R & R RT CREASE BEAM WEB BS 727E-727F IAW SRM 51-40-02-0G-0, W 1.5", O .032", R .023", L1, D .009".

Part: CREASE BEAM — CORRODED (BS 727F-727G) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

RIGHT CREASE BEAM WEB IS CORRODED, BS 727F-727G. ACFT GROUNDED. R & R RT CREASE BEAM WEB BS 727F-727G IAW SRM 51-490-02-0G-0, W 3, O .032, R .026, L 2, D .006.

Part: CREASE BEAM — CORRODED (BS 747-767) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

RIGHT CREASE BEAM WEB IS CORRODED, BS 747-767. ACFT GROUNDED. CORROSION FOUND TO BE OUT OF LIMITS. R & R WEB IAW SRM 51-40-02-0G-0, W 2, O .032, R .027, L 1, D .005.

Part: FAILSAFE — CORRODED (BS 827) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

AFT PIT FRAME BS 827 FAILSAFE ANGLE IS CORRODED BS 25L TO 23L. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-A-1 DETAIL II. R & R FAILSAFE ANGLE IAW SRM 51-40-02-0G-0, W 1", O .045", R .038:", L 2.00", D .007".

Part: TRANSITION PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

AFT CARGO LT TRANSITION PANEL HAS SPOTS OF CORROSION, BS 767 TO BS 787. ACFT GROUNDED. REMOVED CORROSION WAS FOUND OUT OF LIMITS, REPAIRED TRANSITION IAW SRM 53-60-53-2R-4, W 1.5, O .080, R .034, L 1.2, D .006.

Part: FRAME — CORRODED (BS 887) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

AFT CARGO BAY FRAME BS 887 IS CORRODED ON AFT SIDE AT LBL2. ACFT GROUNDED. REMOVED CORROSION, WAS FOUND OUT OF LIMITS. REPAIRED FRAME IAW EA 400, 53EA 15774.

Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 69,915 hrs · 40,014 cycles

AFT CARGO BAY STRINGER CLIP, BS 727B, STR 25L IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP, BS 727B, STR 25L IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.

Part: SKIN — CRACKED (BS 963-965) · airframe 69,915 hrs · 40,014 cycles

L2 DOOR CUTOUT FWD LWR CORNER FUSE SKIN IS CRACKED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01-2R-32, DETAIL IV THIS IS A CATEGORY B REPAIR INITIAL THRESHOLD IS SET AT 66,000 CYCLES INTERVALS SET AT 24,000 CYCLES, SRM 53-00-01-212-32, TABLE IX FOR INSPECTION METHODS.

Part: FLOOR PANEL — CORRODED (BS 500C-500G) · corrosion level 2 · airframe 69,915 hrs · 40,014 cycles

FWD CARGO NR 4 FLOOR PANEL IS CORRODED. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05-0G-0.

Part: TORQUE BOX — CRACKED · airframe 69,915 hrs · 40,014 cycles

APU TORQUE BOX RT SIDE INLET DUCT CORRODED AROUND THE FASTENER HOLES TOP STRAP. ACFT GROUNDED.

Part: DOOR — OUT OF ADJUST (L1) · airframe 66,983 hrs · 38,198 cycles

F/E REPORTS L1 DOOR IS DIFFICULT TO CLOSE. ACFT GROUNDED. VERFIED L1 DOOR DIFFICULT TO CLOSE, TRIED ADJUSTING SNUBBER, NO HELP. RETURNED TO ORIGINAL POSITION. DOOR CLOSED FULLY AT APPROXIMATELY 950 IN/LBS REF MM 52-11-00-755-051. L1 DOOR APPEARS TO HAVE A NEW SEAL POSSIBLY CONTRIBUTING TO THE DIFFICULTY TO CLOSE DOOR. ADJUSTED L-1 DOOR VIA STOP PADS, GUIDE ARM AND HORIZONTAL ROD ADJUSTMENT. HANDLE CLOSING TORQUE 850 IN/LBS. ACCEPTABLE IAW EA 400-52EA-12988, REF MM 52-11-00-705-007.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 66,906 hrs · 38,158 cycles

LEFT HORIZONTAL STABILIZER LOWER AFT THRUST BEAM FITTING CRACKED FOUND DURING INSPECTION IAW TASK CARD SB737-55-1091400-1, STEP 10, FIG 1, STEP 2. ACFT GROUNDED. R & R AND INSPECTED LT HORIZONTAL THRUST BEAM FITTINGS IAW CARD SB737-55-1091-400-2 AND EA 400-55EA-12932.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 66,906 hrs · 38,158 cycles

LEFT HORIZONTAL STAB LOWER AFT THRUST BEAM FITTING CRACKED. FOUND DURING INSPECTION IAW TC SB737-55-1091400-1 STEP 10, FIG 1, STEP 2. ACFT GROUNDED. R & R AND INSPECTED LT HORIZONTAL THRUST BEAM FITTINGS IAW CARD SB737-55-1091-400-2 AND EA 400-55EA-12932.

Part: SKIN — CRACKED (BS 291) · airframe 66,906 hrs · 38,158 cycles

FUSELAGE SKIN IS CRACKED AT R1 DOOR LOWER HINGE CUTOUT. ACFT GROUNDED. REPAIRED DAMAGE TO SKIN IAW EA AD 20140521-400-53-105.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 66,906 hrs · 38,158 cycles

RIGHT WING NR 5 SLAT OTBD CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED RT WING NR 5 SLAT OTBD UPPER CORNER IAW SRM 51-70-10-2R-0, REPAIR 4.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 66,906 hrs · 38,158 cycles

LEFT WING NR 3 SLAT OTBD CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-0, REPAIR 4.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 66,906 hrs · 38,158 cycles

RT WING NR 5 SLAT OTBD CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-0, REPAIR 4.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 66,906 hrs · 38,158 cycles

LT WING NR 3 SLAT OTBD CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED LT WING NR 3 SLAT OTBD UPPER CORNER IAW SRM 51-70-10-2R-0, REPAIR 4.

Part: FRAME — CRACKED (BS 520) · airframe 66,906 hrs · 38,158 cycles

FRAME BS 520 RT SIDE HAS A CRACK. ACFT GROUNDED. REPAIRED IAW SRM IAW SRM 53-00-07-2G-13.

Part: FRAME — CRACKED (BS 440) · airframe 66,906 hrs · 38,158 cycles

FRAME BS 440 IS CRACKED S24R EXTENDING UNDER PAD APPROXIMATELY 1.25 INCH. ACFT GROUNDED. R & R FRAME IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 500G) · airframe 66,906 hrs · 38,158 cycles

FRAME BS 500G RT SIDE HAS CRACK AT ONE INCH WIRE PENETRATION HOLE APPROX .1200 INCH LONG EXTENDING INBD. ACFT GROUNDED. REPAIRED IAW SRM IAW SRM 53-00-07-22-13.

Part: FRAME — CRACKED (BS 500G) · airframe 66,906 hrs · 38,158 cycles

FRAME BS 500G CRACKED. ACFT GROUNDED. REPAIRED IAW SRM IAW SRM 53-00-07-22-13.

Part: FRAME — CRACKED (BS 520) · airframe 66,906 hrs · 38,158 cycles

FRAME BS 520, RT SIDE HAS CRACK AT ONE INCH WIRE PENETRATION HOLE APPROXIMATELY .1200 INCHES LONG EXTENDING INBD. ACFT GROUNDED. REPAIRED IAW SRM IAW SRM 53-00-07-2G-13.

Part: FRAME — CRACKED (BS 440) · airframe 66,906 hrs · 38,158 cycles

FRAME BS 440 IS CRACKED AT LOWER PAD S24R EXTENDING UNDER PAD APPROX 1.25 INCHES. ACFT GROUNDED. R & R FRAME IAW SRM 51-40-02-0G-0.

Part: DOOR — OUT OF ADJUST (L1) · airframe 66,476 hrs · 37,914 cycles

L1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. PERFORMED FWD ENTRY DOOR TEST REF TASK 52-11-00-75-051 DOES NOT PASS TORQE TEST. L1 DOOR WAS ADJUSTED. INSTALLED DOOR LINER AND HANDLE AND L1 SLIDE REF MM 25-61-35-402-003 AND MM 52-11-31-409-009. HANDLE TORQUED WITHIN LIMITS.

Part: FRAME — CORRODED (BS 927) · corrosion level 2 · airframe 66,446 hrs · 37,897 cycles

AFT CARGO FRAME, BS 927, S25-26L CORRODED. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-8.

Part: FRAME — CORRODED (BS 807) · corrosion level 2 · airframe 66,446 hrs · 37,897 cycles

AFT CARGO BAY FRAME BS 807 BETWEEN S27R-27L CORRODED. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-17.

Part: CARGO TRACK — CORRODED (BS 794.3-847) · corrosion level 2 · airframe 66,446 hrs · 37,897 cycles

RIGHT CARGO TRACK CORRODED AT CARGO DOOR OPENING, AFT. ACFT GROUNDED. CARGO TRACK REMOVED IAW SRM 51-40-02. INSTALLED NEW CARGO TRACK AND 2 SPLICES IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 747) · corrosion level 2 · airframe 66,446 hrs · 37,897 cycles

AFT CARGO FLOOR SUPPORT, BS 747, LBL 12.5 CORRODED AT SPLICE. ACFT GROUNDED. FABRICATED NEW PARTS IAW SRM 51-40-02. INSTALLED REPAIR IAW SRM 53-00-53-2R-2, REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (BS 747-767) · corrosion level 2 · airframe 66,446 hrs · 37,897 cycles

AFT CARGO BAY FLOOR SUPPORT, BS 747+4.5 CORRODED ON LOWER SURFACE, LBL 8.10. ACFT GROUNDED. REMOVED CORRODED SECTION AND INSTALLED NEW FLOOR SUPPORT IAW SRM 53-00-53-2R-2, REPAIR 2.

Part: SKIN — CRACKED (BS 727E) · airframe 64,693 hrs · 36,820 cycles

FUSELAGE SKIN CRACKED BS 727E AND S22L. REPAIRED IAW SRM 53-00-01-2R-31 DETAIL VII.

Part: GIRT BAR — CRACKED · airframe 63,497 hrs · 36,073 cycles

L1 DOOR ESCAPE SLIDE GIRT BAR ARM CRACKED. REPAIRED IAW EA400-25EA-09973, REV NEW.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 63,497 hrs · 36,073 cycles

LT HORIZONTAL STAB LOWER SKIN INBD END AT T/E SPAR RIVETS SMOKING. APPEAR TO BE PULLING THROUGH SKIN. REPAIRED SKIN IAW SRM 55-10-01, FIG 202, DETAIL III.

Part: DOUBLER — DAMAGED (BS 1064-1156) · airframe 63,497 hrs · 36,073 cycles

TAILCONE AREA, LT SIDE STRAP ABOVE EDGE OF APU ACCESS DOOR. AFT END OF STRAP IS BENT AT RIVETS. REMOVED, FABRICATED AND INSTALLED NEW STRAP ABOVE EDGE OF LT APU ACCESS DOOR IAW SRM 51 40 02 AND 51 40 05.

Part: SKIN — CRACKED (KRUEGER FLAP) · airframe 63,497 hrs · 36,073 cycles

RIGHT L/E CRACKING AT K-FLAP CUTOUT OTBD EDGE OF K-FLAP. REPAIRED RT OTBD K-FLAP L/E IAW ASA TYPICAL EA 5740-01310.

Part: SKIN — CRACKED (BS 727D) · airframe 63,497 hrs · 36,073 cycles

FUSELAGE SKIN HAS SUBSURFACE CRACK AT CHEM MILL LT STA 727D 2.5 INCHES BELOW STR 23L, APPROX .75 INCHES LONG. REPAIRED SKIN IAW SRM 53-00-01 REPAIR 31. THIS REPAIR IS A CAT B REPAIR.

Part: SKIN — DAMAGED (BS 727G) · airframe 63,497 hrs · 36,073 cycles

SCRIBE LINE AT BS 727G SKIN BUTT STRAP FROM STRINGER 5R TO 6R. R & R WITH NEW BUTT STRAP IAW SRM 51-40-02.

Part: WEB — CORRODED (LT MLG DOOR) · airframe 63,497 hrs · 36,073 cycles

LEFT MLG INNER DOOR WEB IS CORRODED. INSTALLED NEW WEB IN LT MLG INNER DOOR.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 63,497 hrs · 36,073 cycles

LEFT OTBD FOREFLAP L/E CHAFED ON INBD END. REPAIRED IAW SRM 57-53-01, FIG 101.

Part: SKIN — DENTED (BS 516) · airframe 63,497 hrs · 36,073 cycles

RT FUSELAGE STA 516 SKIN HAS TWO DENTS AT 23R. REPAIRED SKIN DAMAGED IAW SRM 53 00 01, FIG 201, REPAIR 31 DET X.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 63,497 hrs · 36,073 cycles

LEFT WING OTBD MIDFLAP LOWER SURFACE SKIN IS CHAFFED INBD OF NR 1 FLAP TRACK FAIRING. ACFT GROUNDED. REPAIRED LT WING OTBD MIDFLAP LOWER SKIN IAW EA CMPT-57EA-09933.

Part: FLOOR SUPPORT — CORRODED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, FIG 101. FABRICATED NEW FLOOR SUPORT IAW B DWG 65C26459 AND SRM 51-40-05, FIG 2.

Part: ANGLE — CRACKED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

ANGLE IS CRACKED AT BS 727D. REMOVED ANGLE. FABRICATED NEW IAW DWG 65-49917 AND INSTALLED NEW ANGLE IAW SRM 51-40-02, PG 6, PAR D.

Part: ANGLE — CRACKED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

ANGLE CRACKED AT BS 727D. R & R ANGLE IAW SRM 51-40-02, PG 6.

Part: ANGLE — CRACKED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

ANGLE CRACKED AT BS 727D. R & R ANGLE IAW SRM 51-40-02, PG 6.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · airframe 63,010 hrs · 35,762 cycles

FLOOR SUPPORT CORRODED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, FIG 101, DETAIL V, FABRICATED NEW FLOOR SUPPORT IAW B DWG 65C26459 AND SRM 51-40-05, FIG 2.

Part: FLOOR SUPPORT — CORRODED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-60-53, FIG 101. FABRICATED NEW FLOOR SUPPORT IAW B DWG 65C26459 AND SRM 51-40-05, FIG 2.

Part: ANGLE — CRACKED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

ANGLE CRACKED AT BS 727B, REMOVED ANGLE, FABRICATED NEW IAW DWG 65-49917 AND INSTALLED NEW ANGLE IAW SRM 51-40-02, PG 6, PAR D.

Part: CHANNEL — CRACKED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

AFT PIT CHANNEL BETWEEN STR 28L AND 28R AT STA 727 D IS CRACKED. REMOVED, FABRICATED NEW CHANNEL IAW DWG 65-65710. INSTALLED NEW CHANNEL IAW SRM 51-40-02, PG 6, PAR D AND PG 2, PAR 4.

Part: ATTACH FITTING — CRACKED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

AFT PIT TWO GUSSETS ATTACHED TO 727D FRAME CRACKED. REMOVED GUSSETS. FABRICATED NEW IAW B DWG 65-65710 AND SRM 51-40-05, FIG 2. INSTALLED NEW GUSSETS IAW SRM 51 40 02. P66 PAR D.

Part: ATTACH FITTING — CRACKED (BS 727D) · airframe 63,010 hrs · 35,762 cycles

AFT PIT, TWO GUSSETS ATTACHED TO 727D FRAME CRACKED. REMOVED GUSSETS. FABRICATED NEW IAW B DWG 65-65710 AND SRM 51-40-05, FIG 2. INSTALLED NEW GUSSETS IAW SRM 51 40 02, P66, PAR D.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 62,911 hrs · 35,703 cycles

MID CABIN LEFT EMERGENCY EXIT SIGN FELL OFF. SECURED MID CABIN LT SIDE EMERGENCY EXIT SIGN LENS.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 62,535 hrs · 35,466 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE OVER OVERWING EXITS AND LEFT OVERWING AFT EXIT DOOR. R & R BAD BATTERY PACK M1576. OPS CKS NORMAL IAW AMM 33-51-51-962-015.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,796 hrs · 34,433 cycles

FRAME AT 500E RIGHT IS CRACKED AT WIRE PENETRATION HOLE I/B SIDE. REPAIRED FRAME IAW 737 400 SRM 53 00 07 REP 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,796 hrs · 34,433 cycles

FRAME AT 500E IS CRACKED AT WIRE PENETRATION HOLE I/B SIDE. REPAIRED FRAME IAW 737 400 SRM 53 00 07 REP 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,796 hrs · 34,433 cycles

FRAME AT 500B LEFT IS CRACKED AT WIRE PENETRATION HOLE I/B SIDE. REPAIRED FRAME IAW B737 400 SRM 53 00 07 REP 13.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,667 hrs · 34,372 cycles

WHILE OPS TESTING EMER EXIT LIGHTS FOUND R1 DOOR EXIT LIGHT INOP OUTSIDE. RELAMPED R1 OUTSIDE EXIT LIGHT & OPS TEST GOOD REF MM 33 51 02.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 60,224 hrs · 34,114 cycles

EMERGENCY EXIT ROW OVERHEAD EMERGENCY EXIT SIGN DID NOT ILLUMINATE WHEN GROUND POWER DROPPED OFF LINE. ALL OTHER EMERGENCY EXIT SIGN ILLUMINATED. RECYCLED ACFT POWER OPS CHECK NORMAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,871 hrs · 33,351 cycles

CRACK FOUND IN E BAY INTERCOSTAL BS 344 TO BS 360 BL 0 WL 200. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW B737 400 SRM 51 40 02, 51 40 05, 51 20 01.

Part: STRAP — CRACKED (E&E BAY) · airframe 58,871 hrs · 33,351 cycles

FOUND STABILIZING STRAP IN E BAY BROKEN BS 312 BL 0 WL 200. REMOVED AND REPLACED STABILIZING STRAP IAW B737 400 SRM 51 40 02, 51 40 05, 51 20 01.

Part: DOOR — OUT OF ADJUST (L2) · airframe 58,009 hrs · 32,868 cycles

FA'S REPORT L 2 DOOR MORE DIFFICULT TO OPEN THAN NORMAL. ADJUSTED L 2 DOOR PER B737 400 MM 52 13 31.

Part: HINGE FITTING — LACK OF LUBE (L2 DOOR) · airframe 57,496 hrs · 32,597 cycles

FLIGHT ATTENDANT REPORTED L2 EXIT DOOR IS DIFFICULT TO OPEN LUBED DOOR HINGES, OPS NORMAL AMM 52 13 00 705 003.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FWD CARGO COMPARTMENT FRAME CLIP HAS CORROSION. REMOVED AND INSTALLED NEW ANGLE.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

STR 5R CLIP CRACKED AT STA 727C. REMOVED AND REPLACED STR CLIP.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

APU COMPARTMENT APU INLET DUCT ATTACH FLANGE IS CORRODED ON I/B SIDE. REMOVED AND REPLACED WITH NEW STRINGER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME STA 867 STR 26R TO 25R SHEAR TIE IS CORRODED. REPAIRED SHEAR TIE.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

STR 4R CLIP CRACKED AT STA 867. REMOVED AND REPLACED WITH NEW CLIP.

Part: SPOILER — DENTED (LT WING) · airframe 57,323 hrs · 32,494 cycles

LEFT WING T/E AND NR 1 SPOILER UPPER T/E DENTED I/B OF O/B END. REPAIRED DAMAGE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

FOUND CORROSION ON INTERNAL AND EXTERNAL SKIN. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

SHEAR TIE AT STA 867 HAS CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 787. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 440. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 747. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 380. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

APU LOWER TORQUE BOX INLET CUTOUT LOWER INBOARD FLANGE CORRODED. REMOVED DAMAGED LOWER STRINGER AND INSTALLED NEW.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

RIGHT O/B SEAT TRACK HAS LUG DAMAGED. REMOVED AND INSTALLED NEW.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

STR 5R CLIP CRACKED AT STA 727D. REMOVED AND REPLACED CLIP.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

RIGHT O/B SEAT TRACK HAS MISSING LOBE. REMOVED AND INSTALLED NEW.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

RIGHT I/B SEAT TRACK HAS GOUGES. REMOVED AND INSTALLED NEW.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

SHEAR TIE AT STA 827 HAS CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

STRINGER CLIP STA 639 STR 2R IS CRACKED. REMOVED CRACKED CLIP AND INSTALLED NEW STRINGER CLIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

STRINGER CLIP CRACKED AT STA 500F AND STRINGER 25L. REMOVED CRACKED CLIP AND INSTALLED NEW STRINGER CLIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 500F. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 787R. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

LEFT O/B SEAT TRACK HAS SEVERAL GOUGES. REMOVED AND INSTALLED NEW.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 747R. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

RIGHT O/B SEAT TRACK HAS SEVERAL GOUGES. REMOVED AND REPLACED WITH NEW.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

STA 947.5 FLOORBEAM HAS CORROSION AROUND FASTENER HOLES AT RBL 6. REPAIRED AFT FLANGE OF FLOORBEAM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 440. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 867. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 907. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 400. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

LEFT I/B SEAT TRACK HAS SEVERAL GOUGES. REMOVED AND INSTALLED NEW.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 827. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME CRACKED AT STA 727F. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: RIB — CRACKED (RT WING) · airframe 57,323 hrs · 32,494 cycles

RT WING RIB LOWER CHORD AT WING STA 135 IS CRACKED. REPAIRED RIB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FLOOR FRAME STA 380 CORRODED ON TOPSIDE. REMOVED DAMGE AND INSTALLLED REPAIR PARTS.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FWD SIDE INTERCOSTAL ATTACH CLIP FROM FRAME TO INTERCOSTAL AT STR 11L IS CRACKED. REMOVED AND INSTALLED NEW.

Part: WEB — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FLOOR WEB AT STR 17L CORRODED AT STA 807. REMOVED DAMAGED AREA AND INSTALLED NEW PART.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

STA 1006 22R FRAME HAS CORROSION AT STRINGERS ATTACHMENT. REPAIRED FRAME.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

AFTER ROMOVAL OF FRAME FOUND STRINGER CLIP AT STA 847 STR 27R CRACKED. REMOVED AND INSTALLED NEW.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

AFT CARGO EQUIPMENT BAY STA 968 STR 25L CORRODED FWD END. REMOVED CORROSION AND INSTALLED REPAIR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

AFT CARGO BAY STA 986 FRAME CLIP CORRODED ON AFT SIDE OF FRAME. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

AFT LAV DRAIN MAST DOUBLER CHANNEL CORRODED AT FS 998. REMOVED AND REPLACED AFT LAV DRAIN MAST.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

LT AND RT REPAIR SECTIONS ON T-CAP ARE CORRODED STA 986. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

STR 27 AT STA 847 CORRODED. REMOVED DAMAGED AREA AND INSTALLED REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FWD CARGO COMPARTMENT FRAME AT STA 500D HAS DENT ABOVE STR 24L. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

R2 LOWER SILL INNER CHORD CORRODED. REPLACED LOWER SILL INNER CHORD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

REINFORCEMENT ANGLE AT 747 FRAME AND STR 27L IS CORRODED. REMOVED AND REPLACED ANGLE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

STA 967 CORRODED AT STR 25R TO 23L. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

STA 1006 STR 22L FRAME HAS CORROSION. REMOVED DAMAGE AND INSTALLED REPAIR PARTS.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

CORROSION ON APB INNER SKIN. REPAIRED APB WEB.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

RT CUSP WEB AT STA 847 - 867 CORRODED. REMOVED CORROSION AND INSTALLED REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

CORROSION ON APB LT AND RT FRAME CHANNEL AT BL 0. REPAIRED CHANNELS.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

MAIN CABIN FLOOR AT L2 DOOR CREASE BEAM AND ANGLE IS CORRODED. REPLACED CREASE BEAM AND ANGLE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

AFT CARGO SHEAR TIE AT STA 767 BETWEEN STR 27L CORRODED. REMOVED CORROSION AND INSTALLED REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

STA 500F IB OF 28L CORRODED. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

STA 500G FRAME CLIP CORRODED. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME AT STA 727C LOWER LEG CORRODED BETWEEN STR 25L AND 26L. REPAIRED FRAME.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

AFT PIT SHEAR TIE AT STA 927 HAS CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

AFT CARGO ANGLE AT STRINGER 25R HAS CORROSION. FABRICATED NEW PART AND INSTALLED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME AT STA 727D LOWER LEG CORRODED BETWEEN STR 25L AND 26L. REPAIRED FRAME.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

AFT PIT SHEAR TIE AT STA 927 HAS CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME AT STA 747 CORRODED ON LOWER LEG. REMOVED CORROSION AND INSTALLED REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,323 hrs · 32,494 cycles

FRAME REPAIR AT FS 747 CORRODED. REPAIRED FRAME.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

AFT CARGO SHEAR TIE IS CORRODED AT FS 807. REPAIRED SHEAR TIE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

FRAME AT STA 847 STR 25R CORRODED. REMOVED AND REPLACED FRAME.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 57,323 hrs · 32,494 cycles

LT WING I/B LEADING EDGE HAS CRACKED INTERCOSTAL ON LOWER SURFACE. REMOVED SUPPORT ANGLE AND INSTALLED REPAIR PARTS.

Part: SILL — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

AFT PIT ENTRY SILL WEB CORRODED AROUND LOWER FASTENER HOLES. REPAIRED WITH NEW PART.

Part: SKIN — DENTED (SPOILER) · airframe 57,323 hrs · 32,494 cycles

NR 2 SPOILER UPPER SURFACE HAS PROTRUDING DENTS. REPAIRED NR 2 SPOILER.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

BEAR STRAP CORRODED FS 847. REPAIRED AFT CARGO BEAR STRAP.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,323 hrs · 32,494 cycles

LT FUSELAGE DENTED FS 727E+14 AND 727F+4. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS.

Part: DOOR — DEFECTIVE (R2) · airframe 56,235 hrs · 31,862 cycles

F/A REPORTS R2 DOOR DIFFICULT TO CLOSE. REMOVED OLD DOOR AND INSTALLED SERVICEABLE DOOR RIGGED AND OPS TESTED GOOD REF MM 52 41 00 404 012 STEP F [1] THRU F [9] D.

Part: SKIN — GOUGED (BS 903-920) · airframe 55,031 hrs · 31,122 cycles

FOUND SKIN DAMAGE TO LT AFT FUSELAGE FWD OF L2 DOOR THRESHOLD. CUTOUT DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER AND FILLER.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

NR 8 FLAP TRACK AFT ATTACH POINT RUSTY AT SHIMS. REMOVED AND REPLACED THE NR 8 FLAP TRACK.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

NR 6 FLAP TRACK IS CORRODED ON BEARING WEAR SURFACES. REMOVED AND REPLACED NR 6 FLAP TRACK.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

NR 2 FLAP TRACK HAS EVIDENCE OF CORROSION ON ALL ROLLER SURFACES. REMOVED AND REPLACED NR 2 FLAP TRACK.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

NR 1 FLAP TRACK AT AFT O/B MOUNT BOLT HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED NR 1 FLAP TRACK.

Part: SKIN — GOUGED (NR 1 PYLON) · airframe 54,479 hrs · 30,809 cycles

NR 1 PYLON PANEL 5727L CUTOUT SKIN FWD EDGE IS GOUGED FROM PANEL. BLENDED AREA, FOUND OUT OF LIMITS. ACCOMPLISHED REPAIR TO THE NR 1 ENG PYLON PANEL CUTOUT.

Part: SUPPORT BRACKET — CRACKED (ENTRY DOOR) · airframe 54,479 hrs · 30,809 cycles

FWD ENTRY DOOR LWR FWD LINER SUPPORT BRACKET IS CRACKED AT STOP PIN FITTING. REMOVED AND REPLACED FWD ENTRY DOOR FWD LINER SUPPORT BRACKET.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 54,479 hrs · 30,809 cycles

FWD ENTRY DOOR LWR AFT LINER SUPPORT BRACKET IS CRACKED AT STOP PIN FITTING. REMOVED AND REPLACED FWD ENTRY DOOR AFT LINER SUPPORT BRACKET.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 54,479 hrs · 30,809 cycles

RIGHT O/B FORE FLAP TRAILING EDGE UPPER SURFACE IS DELAMINATED. REPLACED O/B FORE FLAP.

Part: HOUSING — CRACKED (HORIZ STAB) · airframe 54,479 hrs · 30,809 cycles

HORIZONTAL STAB FWD MECHANISM CRACKED LOWER FLANGED. REMOVED AND REPLACED HOUSING.

Part: SKIN — GOUGED (LT WING) · airframe 54,479 hrs · 30,809 cycles

LEFT WING LOWER SURFACE TRAILING EDGE PANEL JUST OUTBOARD OF THE NR 3 FLAP TRACK FAIRING IS GOUGED ON INNER SURFACE OVER CONE AREA. REPAIRED GOUGE ON INNER SURFACE OVER CONE AREA ON LEFT WING LOWER SURFACE TRAILING EDGE JUST OUTBOARD OF THE NR 3 FLAP TRACK FAIRING IAW SRM.

Part: SUPPORT ANGLE — CHAFED (APU DOOR) · airframe 54,479 hrs · 30,809 cycles

APU COMPARTMENT DOOR LATCH FWD HOLE CHAFED. REPAIRED APU COMPARTMENT DOOR LATCH FWD STRUCTURE SUPPORT ANGLE FOUND OUT OF LIMITS.

Part: SKIN — CHAFED (TE FLAP) · airframe 54,479 hrs · 30,809 cycles

RIGHT O/B FORE FLAP I/B LEADING EDGE IS CHAFED. REPAIRED IAW SRM.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

NR 3 FLAP TRACK HAS EVIDENCE OF CORROSION ON ALL ROLLER SURFACES. REMOVED AND REPLACED NR 3 FLAP TRACK.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

NR 7 FLAP TRACK AFT ATTACH POINT RUSTY AT SHIMS. BOLT HOLES WERE FOUND TO BE CORRODED TRACK WAS REMOVED AND REPLACED.

Part: SKIN — CHAFED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

CHAFING OF FUSELAGE SKIN COMMON TO DORSAL FIN BETWEEN 2L 2R BS 861 887. REPAIRED SKIN.

Part: WEDGE — CHAFED (TE FLAP) · airframe 54,479 hrs · 30,809 cycles

RIGHT I/B MID FLAP TRAILING EDGE WEDGE O/B CONTROL ROD CUTOUT IS CHAFED. REPAIRED IAW SRM.

Part: WEDGE — CHAFED (TE FLAP) · airframe 54,479 hrs · 30,809 cycles

RIGHT I/B MID FLAP TRAILING EDGE WEDGE I/B CONTROL ROD CUTOUT IS CHAFED. REPAIRED IAW EA.

Part: GATE — DENTED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

AFT ENTRY DOOR LOWER GATE DENTED ON AFT SIDE. REPLACED AED LOWER GATE.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

FCB AFT BULKHEAD FLOOR TO BULKHEAD SUPPORT ANGLE ASSY IS CORRODED. REMOVED AND REPLACED AFT BULKHEAD FLOOR TO BULKHEAD SUPPORT ANGLE.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

ZEE CHANNEL SHIELD IS PUNCTURED AND CRACKED. REMOVED AND REPLACED CHANNEL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

CRACK IN FRAME I/B INNER CHORD AT FASTENER. REPAIRED FRAME IB INNER CHORD.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

FWD ENTRY DOOR BEAM LOWER GATE STOP DRILL FOR CRACK LEFT NO EDGE MARGIN TO FASTENER HOLE COMMON TO STOP FITTING. REMOVED DAMAGE FROM LOWER BEAM, INSTALLED REPAIR ANGLES.

Part: FITTING — CRACKED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

FOUND CRACK ON AFT ENTRY DOOR SURROUND FITTING. REMOVED AND REPLACED AFT ENTRY DOOR SURROUND SEAL FITTING.

Part: SKIN — CHAFED (RT TE FLAP) · airframe 54,479 hrs · 30,809 cycles

RIGHT OB AFT FLAP LEADING EDGE SKIN IS CHAFED JUST IB OF NR 1 RT OB AFT FLAP REPLACED WITH SERVICEABLE UNIT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

UPPER ANGLE OF INTERCOSTAL IS CRACKED AT FASTENER HOLES. REMOVED AND REPLACED UPPER ANGLE

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,479 hrs · 30,809 cycles

SEAT TRACK CORRODED. REPAIRED SEAT TRACK.

Part: SKIN — WORN (LE SLAT) · airframe 54,479 hrs · 30,809 cycles

NR 2 SLAT T/E WEDGE WORN THROUGH LOWER SKIN I/B END. REPAIRED NR 2 SLAT T/E WEDGE ON I/B END LOWER SURFACE.

Part: DOUBLER — CHAFED (LE SLAT) · airframe 54,479 hrs · 30,809 cycles

NR 3 SLAT T/E WEDGE PREVIOUS REPAIR AT I/B END IS CHAFED. REPAIRED NR 3 SLAT T/E WEDGE AT I/B END.

Part: SILL — CORRODED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

MOPSILL CORRODED BS 315-340 LBL 54 WL 208. REMOVED AND REPLACED MOPSILL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,479 hrs · 30,809 cycles

SEAT TRACK CORRODED BS 346 AND 351 LBL 24 WL 208. REPLACED SEAT TRACK.

Part: HINGE — STIFF (EVAC SLIDE) · airframe 54,283 hrs · 30,693 cycles

R1 DOOR SLIDE DEPLOYED SIDEWAYS DURING TEST. FOUND HINGES ON R1 DOOR ESCAPE SLIDE COMPARTMENT BACKING PAN SHELF VERY STIFF TO MOVE BY HAND. REMOVED AND REPLACED ESCAPE SLIDE COMPARTMENT ASSY WITH NEW SLIDE PACK.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 52,791 hrs · 29,802 cycles

RT STABILIZER LEADING EDGE SKIN HAS DENT ON STA 243 TO STA 254. REMOVED DAMAGE SECTION OF SKIN AND INSTALLED EXTERNAL DOUBLER WITH BLIND FASTENERS PER SRM 55 10 01 REPAIR 3.

Part: ACTUATOR — LEAKING (RT MLG) · airframe 52,631 hrs · 29,715 cycles

RIGHT MAIN GEAR RED RIGHT GEAR LIGHT ON WITH GEAR HANDLE UP. HAD BOTH GREEN AND RED LIGHTS WITH GEAR HANDLE IN OFF POSITION AFTER BEING UP. NORMAL GEAR EXTENSION CHECKED UPLOCK SENSOR GAP REF 32-61-21 WITHIN LIMITS. RANG OUT UPLOCK SENSOR AND 74 RESISTANCE NORMAL REF M/M 32-61-00. REPLACED RT UP LOCK ACTUATOR REF AMM 32-32-41. LUBED MLG (ALL) REF 12-21-11. REMOVED AND REPLACED RT MLG ACTUATOR REF MM 32 32 11. COMPLIED WITH OPS OF MLG TEST REF 32-32-00/715 001. OPS LEAKS CHECKS GOOD.

Part: HINGE — WORN (L1 DOOR) · airframe 51,224 hrs · 28,968 cycles

FA REPORTS L1 IS DIFFICULT TO MOVE OPEN AND CLOSED OPERATED L 1 DOOR AND HEARD AND FELT GRINDING POPPING EMANATING FROM UPPER END OF FUSE TORQUE TUBE INITIATED MIG 2C 224114. WITH FURTHER TROUBLESHOOTING REMOVED L1 DOOR CAM PLATE AND FOUND WORM AREA ON PLATE. ALSO FOUND CRANK ASSEMBLY ROLLER BAD. REMOVED AND REPLACED CRANK ASSEMBLY ROLLER AND CAM PLATE IAW OHM 52 16 01. ASSEMBLED L 1 DOOR IAW AMM 52 11 31. ACCOMPLISHED L 1 FORWARD DOOR OPERATIONAL TEST IAW AMM 52 11 00. OPS CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,832 hrs · 28,773 cycles

AFT PIT CORROSION ON INTERIOR SKIN (BEAR STRAP) UNDER TRANSITION PANEL (ZEE) IN LOWER TORQUE BOX IN FRONT OF CARGO DOOR. REMOVED EXISTING SKIN REPAIR, FABBED REPAIR PARTS AND INSTALLED IAW ASA EA 5330 02334.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,832 hrs · 28,773 cycles

AFT PIT DOOR THRESHOLD AREA HAS MINOR CORROSION BOTTOM OF RBL 22 STA 787 847 (INSIDE LIP OF WEB). REMOVED CORROSION MATERIAL LOSS OF .017 IS OUT OF LIMITS IAW B737 400 SRM 53 60 15 FIG 101. REMOVED AND REPLACED WEB IAW B737 400 SRM 51 40 02 PG 3.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,832 hrs · 28,773 cycles

AFT PIT DOOR CUTOUT STRAP AT STA 795 846 RBL 17 IS CORRODED. STRAP CORRODED OUT OF LIMITS. REPLACED STRAP IAW SRM 51 40 02 PG 2 & 3. ALSO FABBED 65 42949 2 CLIP AND 65 47957 5 WEB. FOUND TO BE DISCREPANT WHEN CHANGING STRAP IAW SRM 51 30 01 PG 7 & 8 AND INSTALLED IAW SRM 51 40 02 PG 2 & 3.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,832 hrs · 28,773 cycles

CORROSION ON BACKSIDE OF FRAME AT STR 25R AT SKIN ATTACH ANGLE STA 767. CUT OUT DAMAGED SECTION OF ATTACH ANGLE AND INSTALLED REPAIR SHEAR TIE AND DOUBLER IAW B737 400 SRM 53 00 07 FIG 201 AND 51 40 02.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 50,832 hrs · 28,773 cycles

AFT PIT REPAIR FOR FRAME AT STA 767 BETWEEN STR 25 26R HAS IMPROPER EDGE DISTANCE. REMOVED IMPROPER REPAIR AND INSTALLED NEW FRAME REPAIR IAW B737 400 SRM 51 70 11 FIG 1 AND 51 40 02.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,832 hrs · 28,773 cycles

STRINGER TIE STA 807 STR 26R IS CORRODED. REMOVED CORRODED STRINGER TIE, FABRICATED AND INSTALLED REPLACEMENT STRINGER TIE IAW B737 400 SRM 51 30 01 AND BOEING DRWG 69 35350.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,832 hrs · 28,773 cycles

STR 25R IS CRACKED AT FASTENER HOLE. REMOVED CRACKED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IAW B737 400 SRM 53 00 03 FIG 201 REPAIR 1.

Part: TAB — DAMAGED (ELEVATOR) · airframe 50,832 hrs · 28,773 cycles

RIGHT ELEVATOR TAB SEPARATING AT HINGE CUTOUTS. REMOVED DAMAGED AREAS, REBONDED HINGE CUTOUT AREAS IAW B737 400 SRM 51 70 17 REPAIR 10.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 50,832 hrs · 28,773 cycles

NR 4 SPOILER HAS SEVERAL DENTS UPPER SURFACE. PREPPED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (T/E FLAP) · airframe 50,832 hrs · 28,773 cycles

LEFT WING I/B FORE FLAP LOWER SIDE HAS MULTIPLE DENTS. PREPPED DENTED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: WEDGE — DENTED (T/E FLAP) · airframe 50,832 hrs · 28,773 cycles

LEFT I/B MID FLAP T/E WEDGE DENTED SEVERAL AREAS. REMOVED DAMAGED SECTIONS OF WEDGE, FABBED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — WORN (L/E SLAT) · airframe 50,832 hrs · 28,773 cycles

NR 3 SLAT T/E LOWER SURFACE SKIN WORN INTO COMPOSITE LAYER. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,832 hrs · 28,773 cycles

DENT IN FUSELAGE SKIN BS 1014 STRINGER 12LT. REMOVED DENTED SECTION OF SKIN, FABRICATED AND BONDED SKIN AND DOUBLER INSTALLED REPLACEMENT SECTION OF SKIN IAW B737 400 SRM 51 70 10 AND BOEING DRWG 65 52988.

Part: WEDGE — CHAFED (L/E SLAT) · airframe 50,832 hrs · 28,773 cycles

NR 4 SLAT T/E WEDGE LOWER SURFACE CHAFED. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CORRODED (BS 867-877) · corrosion level 2 · airframe 49,983 hrs · 28,269 cycles

RIVET HEADS BROKEN OFF AND POSSIBLE CORROSION ON HOLES OF PREVIOUS REPAIR DOUBLER AT STA867 STR 26R. REPAIRED IAW B737 400 SRM 53 00 01 REPAIR 31.

Part: CONTAINER — LACK OF LUBE (R1 DOOR SLIDE) · airframe 49,676 hrs · 28,105 cycles

R1 DOOR EMERGENCY SLIDE TWISTED 90 DEGS DURING DEPLOYMENT AND USE DURING TEST BY FLIGHT CREW. LUBRICATED THE SLIDE CONTAINER LOWER FLAP HINGE (SHELF ASSY) WHICH WAS FOUND TO BE STIFF. SLIDE THEN DEPLOYED PROPERLY.

Part: PLATE — WRONG PART (L1 DOOR) · airframe 47,615 hrs · 26,987 cycles

FLIGHT ATTENDANT REPORTED L1 DOOR HARD TO OPEN FOUND INCORRECT BEARING PLATE INSTALLED WHICH APPEARED TO BE CATCHING ON DOOR DURING LAST 1 INCH OF DOOR CLOSING. AFTER REPLACING PLATE FOUND THE UPPER TORQUE ROD CONTROL LEVER ROLLER NOT ENGAGING CAM AT DOOR HANDLE. RIGGED DOOR, CHECKS GOOD.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 47,584 hrs · 26,973 cycles

THE RIGHT ELEVATOR TAB UPPER SURFACE IS CRACKED AT THE I/B SIDE OF THE SECOND FROM O/B HINGE CUTOUT. PREPARED THE DAMAGED SURFACE FOR BONDING PREPARED AND APPLIED GRAPHITE REPAIR PLIES IAW SRM 51-70-17 REPAIR 11.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 47,584 hrs · 26,973 cycles

THE LEFT NR 4 SPOILER HAS MULTIPLE DENTS ON THE LWR SURFACE FROM THE PANEL CENTER TO THE I/B EDGE. PREPARED THE LWR SURFACE OF THE SPOILER PANEL FOR BONDING FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 47,584 hrs · 26,973 cycles

THE RIGHT ELEVATOR IS DENTED ON THE LWR SURFACE I/B OF THE NR 5 HINGE. REMOVED DAMAGED PLIES FROM LWR SKIN PNL, PREPARED AND APPLIED REPAIR PLIES IAW SRM 51-70-04 PG 4, 33, 37 AND 55, 20, 01 FIG 201.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 47,584 hrs · 26,973 cycles

THE RIGHT O/B AFT FLAP IS DAMAGED ON THE O/B TRAILING EDGE. REMOVED DAMAGED AREA OF T/E ASSY SKIN AND CORE FABRICATED AND INSTALLED A CORE REPAIR SECTION SKIN FILLER AND DOUBLER IAW SRM 51-70-10 PARA 7, 8, 9, 11, 15, 18 AND 20.

Part: SKIN — DENTED (TE FLAP) · airframe 47,584 hrs · 26,973 cycles

THE LEFT I/B FORE FLAP LWR SURFACE HAS MULTIPLE DENTS. PREPARED FORE FLAP ASSY LWR SURFACE FOR BONDING FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW SRM 51-70-10 PARA 7, 8, 12, 15, 18 AND 20.

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 47,584 hrs · 26,973 cycles

THE RIGHT ELEVATOR IS PUNCTURED ON THE UPPER SURFACE 5 INCHES FROM THE T/E AT STA 110. REMOVED THE DAMAGED PLIED FROM THE UPPER SKIN PANEL PREPARED AND APPLIED REPAIR PLIES IAW SRM 51-70-04 PG 4, 33, 37 AND 55-20-01 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON FRAME SHEAR TIE BETWEEN KEEL BEAM AND STRINGER 26R. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53 00 07 AND 51 40 02.

Part: SKIN — BULGED (FUSELAGE) · airframe 43,822 hrs · 24,964 cycles

SKIN BULGING AROUND FASTENERS ALONG STRINGERS 26R AT BSTA 847 AND AT FASTENERS FOR BEAR STRAP BETWEEN STR 26R AND 27R. REPAIRED AREA IAW AS EA 5360 01052 ALONG STRINGERS 26R BSTA 847 AND BEAR STRAP BETWEEN STR 26R AND 27R.

Part: SKIN — DEBONDED (TE FLAPS) · airframe 43,822 hrs · 24,964 cycles

REPAIR ON UPPER SURFACE OF RT IB TE FLAP IS DISBONDED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (TE FLAPS) · airframe 43,822 hrs · 24,964 cycles

LT IB FORE FLAP DENTED 5 INCHES FROM TE AND 15 INCHES FROM IB END ON LWR SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51 70 10.

Part: REPAIR — DELAMINATED (NR 5 SPOILER) · airframe 43,822 hrs · 24,964 cycles

NUMBER 5 SPOILER DELAMINATED ON LWR SURFACE AT EXISTING REPAIR. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53 70 10 REPAIR 4.

Part: FRAME — CRACKED (BS 767) · airframe 43,822 hrs · 24,964 cycles

FRAME AT STA 767 IS CRACKED AT FASTENER HOLE BETWEEN STR 26 27RH. CUTOUT DAMAGED AREA OF FRAME FABRICATED AND INSTALLED REPAIR PIECES PER SRM 51 70 11 FIG 1.

Part: SHEAR TIE — CORRODED (BS 847) · airframe 43,822 hrs · 24,964 cycles

SHEAR TIE CORRODED AT BSTA 847 STR 26 27R. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PIECES PER SRM 53 00 07 FIG 201 REPAIR 10.

Part: SHEAR WEB — CORRODED (BS 847-867) · airframe 43,822 hrs · 24,964 cycles

LT SHEAR WEB IS CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-13 FIG 1.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 43,822 hrs · 24,964 cycles

NUMBER 2 SLAT DELAMINATED I/B SIDE 3 INCHES FROM EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-70-10 REPAIR 4.

Part: SHEAR TIE — CORRODED (BS 500E) · airframe 43,822 hrs · 24,961 cycles

FOUND SHEAR TIE CORRODED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-07 FIG 201 REPAIR 3.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 43,822 hrs · 24,964 cycles

NR 2 SLAT DELAMINATED AT O/B CORNER. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM 51-70-10.

Part: SHEAR WEB — CORRODED (BS 827-847) · airframe 43,822 hrs · 24,964 cycles

LT SHEAR WEB IS CORRODED AT BSTA 827-847. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-13 FIG 1.

Part: FRAME — CORRODED (BS 727C) · airframe 43,822 hrs · 24,964 cycles

FRAME CORRODED AROUND FASTENERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES PER SRM 53-00-07.

Part: FRAME — CORRODED (BS 727D) · airframe 43,822 hrs · 24,964 cycles

FRAME CORRODED AROUND FASTENERS AT BSTA 727D STR 27L-27R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES PER SRM 53-00-07 REPAIR 7.

Part: FRAME — CORRODED (BS 500E) · airframe 43,822 hrs · 24,964 cycles

FOUND FRAME CORRODED AT FASTENER HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-70-11 FIG 1.

Part: SHEAR TIE — CORRODED (BS 500E) · airframe 43,822 hrs · 24,964 cycles

FOUND SHEAR TIE CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-07 FIG 201 REPAIR 3.

Part: SHEAR WEB — CORRODED (BS 360-380) · airframe 43,822 hrs · 24,964 cycles

LT SHEAR WEB IS CORRODED AT BS 360-380. REMOVED DAMAGED FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-70-13 FIG 1.

Part: SHEAR TIE — CORRODED (500E) · airframe 43,822 hrs · 24,964 cycles

FOUND SHEAR TIE CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-07.

Part: WEDGE — DELAMINATED (NR 1 SLAT) · airframe 43,822 hrs · 24,964 cycles

NR 1 SLAT T/E WEDGE HAS 2 EACH AREAS OF DELAMINATION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51-70-10 REPAIR 4.

Part: STRINGER CLIP — BENT (BS 727G) · airframe 43,822 hrs · 24,964 cycles

FOUND STRINGER TIE CLIP BENT. REMOVED TIE CLIP, FABRICATED AND INSTALLED REPLACEMENT TIE CLIP IAW SRM 514002.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,822 hrs · 24,964 cycles

SHEAR TIE CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REAPIR PIECES IAW B737-400 SRM 53-00-07 FIG 201 REPAIR 10.

Part: SHEAR TIE — CORRODED (BS 500B) · airframe 43,822 hrs · 24,964 cycles

SHEAR TIE CORRODED AT BSTA 500B BETWEEN STR 26-27R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-07 REPAIR 10 FIG. 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,822 hrs · 24,964 cycles

SHEAR TIE CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-07 FIG 201, REPAIR 10.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 43,822 hrs · 24,964 cycles

SHEAR TIE CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-07 REPAIR 10 FIG 201.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 43,822 hrs · 24,964 cycles

SHEAR TIE CORRODED AT BSTA 500C BETWEEN STRINGER 26-27LT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PIECES IAW B737-400 SRM 53-00-07 REPAIR 10 FIGURE 201.

Part: GUIDE ARM — OUT OF RIG (L-1 DOOR)

CREW PREFLIGHT - L1 DOOR DIFFICULT TO CLOSE. RIGGED L-1 DOOR GUIDE ARM, CONTROL PUSHROD AND STOP PINS. (K)

Part: STOP FITTING — CORRODED (DOOR) · corrosion level 2

PAE - CORRODED STOP FITTING. REPLACED STOP FITTING. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,028 hrs · 22,889 cycles

PAE - CRACK ON FRAME AT FASTENER BS 359, STR 2L. REPAIRED CRACK IN FRAME AT FASTENER IAW EA. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,028 hrs · 22,889 cycles

PAE - UPPER LOBE, ANGLE CRACKED, BS 292, WL 240, RBL 53. REMOVED AND REPLACED ANGLE. (K)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,028 hrs · 22,889 cycles

PAE - CORROSION FWD GALLEY DOOR CUTOUT (4 EA) THRESHOLD PLATE SUPPORTS. REMOVED AND REPLACED (4 EA) THRESHOLD PLATE SUPPORTS.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,028 hrs · 22,889 cycles

PAE - CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR BS772, RBL 13.80, WL 153. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORIGINAL .070 INCH REMAINING .31 INCH X 1 INCH X 2.5 INCHES. REMOVED AND REPLACED CARGO TRACK FROM BS 727 TO 947.5, RBL 13.8, WL 153. (K)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PAE - AFT CARGO COMPARTMENT TIE DOWN FITTINGS HAVE LIGHT CORROSION. RBL 13.80, STA 947.5 TO 727 RBL 13.8. (K)

Part: STOP FITTING — GOUGED (CARGO DOOR)

PAE - AFT CARGO BAY FWD IB DOOR STOP FITTING IS GOUGED. REPLACED AFT CARGO BAY FWD IB DOOR STOP FITTING. (K)

Part: WEB — SCRATCHED (FUSELAGE) · airframe 40,028 hrs · 22,889 cycles

PAE - FWD CARGO BAY BS 429, RBL 22.5, SCRATCHES ON WEB UNDER FLOOR TO SIDEWALL SUPPORT. BLENDED SCRATCHES, FOUND OUT OF LIMITS, REMOVED AND REPLACED WEB. (K)

Part: DOOR FRAME — CORRODED (DOOR) · corrosion level 2 · airframe 40,028 hrs · 22,889 cycles

PAE - CORROSION ON DOORSILL FWD FRAME. REPLACED FRAME IAW SRM. (K)

Part: SLIDE — FAILED (R1 DOOR)

FOUND R1 ESCAPE SLIDE TEST FAILED. REMOVED AND REPLACED SLIDE PER AMM 25-61-35. THIS SLIDE WAS USED AS PART OF A F/A TRAINING EXERCISE. PRIOR TO DEPLOYING SLIDE A `TARP` WAS AFFIXED TO THE FUSELAGE WITH TAPE TO PROTECT THE PAIN FROM INADVERTENT DAMAGE. THE `TARP` WAS INGESTED INTO THE ASPIRATOR OF THE SLIDE BOTTLE AND ENTANGLED WITH THE SLIDE DURING DEPLOYMENT. THE OVERHAUL OF THE SLIDE WS DONE IAW MANUFACTURES INSTRUCTIONS (CMM 25-66-07 AND EO 2560-00148) AND NO DEFECT WAS FOUND WITH THE SLIDE OR AY ASSOCIATED SUBSYSTEM. THIS SLIDE WAS RETURNED TO SERVICE. (M)

Part: SLIDE — FAILED (R1 DOOR)

PAE - R1 ESCAPE SLIDE TEST FAILED. (SLIDE DEPLOYED, COCKED AT 90 DEGREES) REMOVED AND REPLACED SLIDE IAW AMM. THIS SLIDE WAS USED AS PART OF A F/A TRAINING EXERCISE. PRIOR TO DEPLOYING SLIDE A "TARP" WAS INGESTED INTO THE ASPIRATOR OF THE SLIDE BOTTLE AND ENTANGLED WITH THE SLIDE DURING DEPLOYMENT. THE OVERHAUL OF THE SLIDE WAS DONE IAW MANUFACTURES INSTRUCTIONS, CMM 26-66-07 AND EO 2560-01148, AND NO DEFECT WAS FOUND WITH THE SLIDE OR ANY ASSOCIATED SUBSYSTEMS. THIS SLIDE WAS RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,028 hrs · 22,889 cycles

PAE - CRACKED FRAME. TRIMMED OUT CRACK AND INSTALLED DOUBLER. (K)

Part: STOP FITTING — GOUGED (FUSELAGE)

PAE - AFT CARGO BAY FORWARD INBOARD DOOR STOP FITTING GOUGED. REPLACED AFT CARGO BAY FORWARD INBOARD DOOR STOP FITTING. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

PAE - AFT CARGO BAY FLOOR TO SIDEWALL ANGLE CRACKED. REPLACED CRACKED FLOOR TO SIDEWALL ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - FRAME DAMAGED. REMOVED DAMAGED FRAME, FABRICATED REPAIR, INSTALLED FRAME. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,028 hrs · 22,889 cycles

PAE - STRINGER CLIP CRACKED. REPLACED STRINGER CLIP. (K)

Part: CHANNEL — DENTED (FUSELAGE)

PAE - FOUND CORROSION ON SUPPORT CHANNEL UPPER SURFACE. REMOVED AND INSTALLED NEW SUPPORT CHANNEL. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M)

Part: SUPPORT ANGLE — CORRODED (FLOOR TO WALL) · corrosion level 2 · airframe 40,028 hrs · 22,889 cycles

PAE - CORROSION ON FLOOR TO WALL SUPPORT. REPLACED WALL SUPPORT. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON GALLEY SUPPORT FITTING. REPLACED FITTING. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM. REPLACED PER EA. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SHEAR TIE. REPLACED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AFT CARGO BAY ON FLOOR SUPPORTS AT PREVIOUS REPAIR. BLENDED CORROSION ON FLOOR SUPPORTS, FOUND SEVERAL LOCATIONS OUT OF LIMITS, GENERATED MIG-5'S TO DOCUMENT INDIVIDUAL REPAIRS. (M)

Part: SKIN — GOUGED (FUSELAGE)

PAE - FOUND EXTERNAL FUSELAGE SKIN GOUGE. REPAIRED PER EA. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

PAE - FOUND SEAT TRACK DAMAGED. REPLACED SEAT TRACK. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

PAE - FOUND STIFFENER CORRODED AT APU INTAKE OPENING. REPLACED CORRODED STIFFENER PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - FOUND FUSELAGE UPPER LOBE, AFT ENTRY DOOR MOP SILL CORRODED. REPLACED MOP SILL. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TRACK. REMOVED DAMAGE/CORROSION FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - FOUND STRINGER TIE CRACKED. REPLACED STRINGER TIE. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

FOUND CORROSION ON SHEAR TIE UPPER SURFACE. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SHEAR TIE. REPLACED SHEAR TIE. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

PAE - AFT CARGO TIE DOWN FITTINGS ARE CORRODED. REPAIRED TRACK TIE DOWN FITTING PER SRM. (M)

Part: CHANNEL — DAMAGED (FUSELAGE)

PAE - FOUND DRILL START IN U-CHANNEL ON INTERCOSTAL. REPLACED U-CHANNEL ON INTERCOSTAL. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON HORIZONTAL WEB. REMOVED WEB, FABRICATED NEW WEB, AND INSTALLED. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FRAME TO SKIN ANGLE. REPAIRED PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND FLOOR SUPPORT IS CORRODED. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT. (M)

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE)

PAE - GALLEY SUPPORT CHANNEL IS CORRODED. REMOVED AND REPLACED CHANNEL. (M)

Part: SILL — CORRODED (GALLEY DOOR)

PAE - FOUND CORROSION ON AFT GALLEY DOOR MOP SILL. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M)

Part: SKIN — CRACKED (HORIZONTAL STAB)

PAE - FOUND RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED. CUT OUT DAMAGED SKIN, FABRICATED REPAIR FILLER AND DOUBLER PER SRM AND EA, INSTALLED REPAIR DOUBLER TO LOWER SKIN OF RIGHT HORIZONTAL STABILIZER. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TRACK. REPAIRED FLOOR TRACK. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR TRACK. REPAIRED FLOOR TRACK. (M)

Part: INTERCOSTAL — MISDRILLED (FUSELAGE)

PAE - FOUND INTERCOSTAL IN AFT CARGO BAY MISDRILLED. REPLACED INTERCOSTAL. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. CORROSION FOUND OUT OF LIMITS, REPAIRED FLOORBEAM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - FOUND STRINGER TIE CRACKED. REPLACED STRINGER TIE. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - FOUND DAMAGED SEAT TRACK. REPLACED SEAT TRACK. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM PER SRM. (M)

Part: WEB — GOUGED (FUSELAGE)

PAE - FOUND GOUGES IN VERTICAL WEB. REPLACED WEB. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON GALLEY SUPPORT HAT CHANNEL. REMOVED, FABRICATED AND INSTALLED HAT CHANNEL. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - FOUND FLOOR INTERCOSTAL CRACKED. REPLACED CRACKED INTERCOSTAL. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - FOUND CORROSION UPPER LOBE ON FRAME. FABRICATED AND INSTALLED FRAME. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - FOUND SEAT TRACK IS DAMAGED. REPLACED SEAT TRACK. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

PAE - AFT CARGO BAY SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR STRAP. REPLACED FLOOR STRAP. (M)

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - MECHANICAL DAMAGE ON SEAT TRACK. REMOVED DAMAGED TRACK AND SPLICED IN NEW TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSLEAGE)

PAE - FOUND CORROSION ON SEAT TRACK. REPLACED SEAT TRACK. (M)

Part: SUPPORT — SCRATCHED (FUSELAGE)

PAE - FOUND FORWARD CARGO BAY, SCRATCHES ON WEB UNDER FLOOR TO SIDEWALL SUPPORT. REPLACED WEB. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M)

Part: STRIP — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR STRIP. REPLACED FLOOR STRIP. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - ELONGATED HOLES AND DRILL STARTS. REMOVED AND REPLACED. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM UPPER FLANGE. (M)

Part: WEDGE — DENTED (NR 1 SLAT)

PAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - AFT CARGO BAY FLOOR SUPPORT IS DAMAGED. REPLACED FLOOR SUPPORT. (M)

Part: WEDGE — DENTED (NR 1 SLAT)

PAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M)

Part: FRAME — DAMAGED (FUSELAGE)

PAE - FOUND MECHANICAL DAMAGE ON FRAME. REPAIRED FRAME. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON WEB. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON AFT CARGO BAY, FRAME, FORWARD LOWER ANGLE. REPAIRED DAMAGED FAIL/SAFE L-ANGLE, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PAE - FOUND UPPER LOBE ANGLE CRACKED. REPLACED UPPER LOBE ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - FOUND SKIN DENTED. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION FUSELAGE UPPER LOBE, FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED FLOORBEAM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FOUND CORROSION FUSELAGE UPPER LOBE, FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED FLOORBEAM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PAE - FOUND UPPER LOBE, ANGLE CRACKED. REPLACED PER SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - FOUND LOWER FUSELAGE BELOW AFT CARGO COMPARTMENT BILGE LEFT Z-ANGLE AT STATION 727-847 HAS CORROSION ON THE UPPER SURFACE AT SEVERAL PLACES. MARKED IN RED. REMOVED CORRODED Z-ANGLE ON LEFT SIDE STATION 727-847. INSTALLED NEW Z-ANGLE IN REF SRM 51-40-02 PAGE 3. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE STATION 927-947 RT SHEAR TIE CORRODED. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT, BILGE RT STATION 947 CORRODED AROUND THE DOWN FITTINGS. MARKED DOT 1025. REMOVED CORRODED CARGO TIE DOWN TRACK AND INSTALLED NEW CARGO TIE DOWN TRACK SECTION AND REPAIR SPLICE AT AFT CARGO COMPARTMENT BILGE RT STATION 917-947. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

OAK - FOUND DOOR RT FORWARD SERVICE LOWER AFT FITTING SUPPORT FASTENER HOLE CRACKED INSIDE LOWER DOOR MARKED 1023. SPLICED IN NEW DOOR, FRAME AND INSTALLED DOUBLER AT RT FORWARD SERVICE DOOR LOWER AFT CORNER. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - FOUND LOWR FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE RT Z-ANGLE AT FS 727 TO 787 HAS CORROSION ON THE UPPER SURFACE AT SEVERAL PLACES, MARKED IN RED. REMOVED RT Z-ANGLE AFT CARGO COMPARTMENT FS 727-787. INSTALLED NEW Z-ANGLE FROM FS 727-787. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 25 INOPERATIVE. RECONNECTED WIRE AND OPERATIONAL CHECKED GOOD. (M)

Part: SKIN — BIRD STRIKE (T/E FLAP)

YVR - DURING APPROACH INTO YVR, EXPERIENCED MULTIPLE BIRD STRIKE ON LEFT INBOARD MID FLAP LEADING EDGE. REPAIRED IAW SRM. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

PDX - FOUND EMERGENCY FLOOR LIGHTS ARE INOPERATIVE AT ROWS 14-16. RECONNECTED TRACK LIGHTS. TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: SKIN — CRACKED (LT WING)

SEA - DURING CHECK, FOUND LEFT WING FIXED LEADING EDGE CRACKED JUST INBOARD OF PYLON AT K-FLAP LOCATION. REPAIRED IAW WITH EA. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY SUB THRESHOLD WEB CORRODED. REMOVED AND REPLACED IAW SRM. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING AT ROW 18 AND 25 DISCONNECTED. RECONNECTED TRACK LIGHTS, OPS CHECKED NORMAL. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT AT ROW 14-19 DISCONNECTED. RECONNECTED TRACK LIGHTS, OPERATIONAL CHECK GOOD. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT AT ROW 14-19 DISCONNECTED. RECONNECTED TRACK LIGHTS, OPERATIONAL CHECK GOOD. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND ROW 15C EMERGENCY LIGHTS INOPERATIVE. RECONNECTED TRACK LIGHT, OPERATIONS CHECK NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 13-17. RECONNECTED WIRES, OPS CHECK NORMAL. (M)

Part: WIRE — DAMAGED (CABIN)

SEA - DURING A LINE CHECK, FOUND TWO BANKS OF EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE STARTING AT ROW 18. REPAIRED WIRES AT ROW 18. FLOOR TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: GUIDE — DEFECTIVE (L1 DOOR)

SEA - DURING PREFLIGHT CHECK, FOUND THE L1 DOOR STIFF AND DIFFICULT TO OPEN. REPLACED GUIDE ARM. DOOR THEN OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 13-16. RECONNECTED WIRES AT ROWS 16. FLOOR TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN) · corrosion level 3 · airframe 24,020 hrs · 14,306 cycles

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13-16 WERE FOUND INOPERATIVE. RECONNECTED LOOSE CONNECTOR AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 27 AFT. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL LAMP — FAILED (CABIN)

SEA - ROW 27 DEF EMERGENCY LIGHT ON BULLNOSE INOP. MAINTENANCE RE-LAMPED. (M)