N624AS

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 40,545 hrs · 17,981 cycles

ON WALKAROUND FOUND POSSIBLE CRACK IN RT STAB LOWER SURFACE APPROX STAB STATIONS 147-157. HFEC INSPECTION IAW NDT 51-00-00, PART B CRACK VERIFIED. STAB STA IS 129.5 RT STAB 17 AFT OF L/E SKIN. RT HORZ STAB L/E REMOVED REF 27-41-21-000-801. REMOVED EXTERIOR FINISH AROUND DAMAGED AREA REF AMM 51-21-11-150-801. REPAIRED RT STAB LOWER SURFACE CRACK AS REQUIRED REF SRM 55-10-01, EA 700-55EA-08792. MIG-2C NR 290056 COMPLETED. RT HORZ STAB L/E INSTALLED ON MIG-2C .

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,475 hrs · 17,043 cycles

RIGHT AFT TWO OVERHEAD BIN EMERGENCY LIGHTS FAIL 15 MIN TEST. REMOVED AND REPLACED BATTERY PACK IAW B737NG AMM 33 51 06 960 806. OPS CHECK OF BATTERY PACK GOOD IAW B737NG AMM 33 51 06 960 806. POWER BATTERY CAPACITY CHECK GOOD IAW B737NG AMM 33 51 06 200 801.

Part: BRACKET — CRACKED (LT WING) · airframe 38,476 hrs · 17,043 cycles

LEFT WING T/E CAVITY AT WS 289 SEAL RETAINER BRACKET CRACKED AFT SIDE. REMOVED AND REPLACED IAW B737 700 51 40 02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN FLOORBOARD SUPPORT AT BS 540 BL 0 LBL 24 IS CRACKED. REPLACED FLOORBOARD SUPPORT IAW B737 700 SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN INTERCOSTAL CRACKED AROUND NUT PLATE BS 310 & BS 325 RBL 32. REPLACED INTERCOSTAL IAW B737 700 SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN UNDER FLOOR INTERCOSTAL CRACKED BS 278 - 298 RBL 1. REPLACED INTERCOSTAL IAW B737 700 SRM 51 40 02.

Part: RIB — WORN (RT WING) · airframe 38,476 hrs · 17,043 cycles

RT WING TRAILING EDGE DEFLECTION RIB WORN AT ATTACH FITTING. REPAIRED OVERSIZED ATTACHMENT HOLE COMMON TO LOWER PANEL PART OF THE TAB DEFLECTION CONTROL RIB PER REO G14531 REV A DATE 01 30 2012 AND ASA EA 700 57EA 07330. ADJUSTED UPPER AND LOWER T/E PANELS IAW B737NG AMM 57 50 01 AND 57 50 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN UNDER FLOOR AREA INTERCOSTAL CRACKED AT BS 321 LBL 44. REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL PN 141A541OU12 PO#730264.4 IAW B737 700 SRM 51 40 02 AT STA 321 LBL 44.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

AFT CARGO COMPARTMENT RT STA 771 STR 26 TO STR 27 FLOOR SUPPORT UNDER PANEL CORRODED. REMOVED AND REPLACED FLOOR SUPPORT TEE ASSEMBLY IAW B737 700 SRM 51 40 02 AT STA 771 IN AFT CARGO COMPARTMENT.

Part: TRANS PANEL — CORRODED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

AFT CARGO COMPARTMENT LT STA 727D TO 767 STR 26 TRANSITION PANEL CORRODED AROUND FASTENER HOLES. REPAIRED DAMAGED AREA IAW B737 700 SRM 53 00 53 REPAIR 5 BY FABRICATING AND INSTALLING SIDEPLATE REPAIR AND SPLICE PLACE IAW B737 700 SRM 53 00 53. ALODINED PRIMED AND PAINTED IAW B737 700 SRM 51 20 01 AND B737NG AM 51 21 99.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED IN RADIUS BS 380 BS 420 BL 0. REPLACED MAIN CABIN FLOOR INTERCOSTAL AT STA 380 420 BL 0 IAW B737 700 SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN UNDER FLOOR AREA INTERCOSTAL CRACKED AT BS 335 LBL 45. REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL PN 141A541OU16 PO#705881.3 IAW B737 700 SRM 51 40 02 AT STA 335 LBL 45.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,476 hrs · 17,043 cycles

AFT CARGO COMPARTMENT RT STA 727D STR 26 TOP OF FRAME CORRODED. REMOVED FRAME SPLICE IAW B737 700 SRM 51 40 02 FORMED SPLICE IAW BAC DWG 146A1300 REV A HEAT TREATED FROM 7075 0 TO T6 IAW BAC 5602 AND BM2770J LOCATED AND DRILLED IAW B737 700 SRM 51 40 02 AND BAC DWG 146A1300 REV A ALODINED AND PRIMED IAW B737 700 SRM 51 20 01 INSTALLED SPLICE IAW B737 700 SRM 51 40 02 AND BAC DWG 146A1300 REV A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN FLOORBOARD SUPPORT CRACKED THREE PLACES BS 540 BL 0 RBL 24. REMOVED AND REPLACED FLOORBOARD SUPPORT IAW B737 700 SRM 51 40 02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,476 hrs · 17,043 cycles

AFT CARGO COMPARTMENT RT STA 787 STR 25 TO STR 26 TOP OD FRAME HAS LIGHT CORROSION. REMOVED FRAME SPLICE IAW B737 700 SRM 51 40 02 MAT ID 7075 0 .063 FORMED SPLICE IAW BAC DWG 146A1300 REV A HEAT TREATED FROM 7075 0 TO T6 LOCATED AND DRILLED IAW B737 700 SRM 51 40 02 AND BAC DWG 146A1300 ALODINED AND PRIMED IAW B737 700 SRM 51 20 01. INSTALLED SPLICE IAW B737 700 SRM 51 40 02 AND DWG 146A1300 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN UNDER FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 AND BS 360 LBL 11. REPLACED MAIN CABIN FLOOR INTERCOSTAL BETWEEN STA 344 AND 360 LBL 11 IAW B737 700 SRM 51 40 02.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 38,476 hrs · 17,043 cycles

MAIN CABIN UNDER FLOOR SUPPORT CRACKED BETWEEN BS 344 AND 360 LBL 11. REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02.

Part: RIB — CRACKED (HORIZ STAB) · airframe 38,476 hrs · 17,043 cycles

LT HORIZONTAL STAB STA 92.7 INTERNAL RIB HAS 2EA MACHINED STIFFENERS CRACKED (2ND AND 3RD FROM FRONT AT LOWER LEGS). DISPLACED LT HORIZ STAB FWD WEB BETWEEN STA 66.50 AND 129.50 IAW B737 700 SRM 51 40 02. REMOVED INSPAR RIB AT STA 92.7 REMOVED DAMAGED METAL AT 2 EA CRACKED STIFFENERS AND FABRICATED REPAIR PARTS IAW B737 700 SRM 55 10 09 FIG 202 REPAIR 4. ALODINED AND PRIMED REPAIR PARTS IAW B737 700 SRM 51 20 01. INSTALLED REPAIR PARTS IAW B737 700 SRM 55 10 09. RE-INSTALLED RIB BAC DWG 182A4001 AND REINSTALLED SPAR WEB IAW BAC DWG 182A4081 AND B737 700 SRM 51 40 02.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 37,153 hrs · 16,417 cycles

FORWARD ENTRY DOOR HARD TO CLOSE. OPERATED DOOR IAW MM 52 11 00 860 804, DOOR OPS NORMALLY. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (ENTRY DOOR) · airframe 37,153 hrs · 16,417 cycles

FORWARD ENTRY DOOR HARD TO CLOSE. OPERATED DOOR IAW B737 700 AMM 52 11 00 860 804 DOOR OPERATED NORMALLY OK FOR SERVICE.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 33,643 hrs · 14,766 cycles

HIGH PRESSURE AIR ACCESS DOOR LATCH WEARS INTO LOWER CHORD. FABRICATED AND INSTALLED A REPAIR STRAP AND FILLER.

Part: SHIELD — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT DOOR SURROUND FWD SHIELD HAS SURFACE CORROSION FROM BS 767 TO BS 795 STR 25R. AFT CARGO PIT SHIELD CORROSION BLENDED OUT. BLEND AREA FOUND TO BE BEYOND LIMIT. SHIELD REPLACED WITH REPAIR PART IAW B737 700 SRM 53 60 15 AND 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT PASSENGER CABIN CORROSION ON FLOORBEAM AT BS 986 RBL 12. CORROSION ON FLOORBEAM BLENDED OUT BLEND AREA FOUND TO BE BEYOND LIMIT. FLOORBEAM REPAIRED IAW B737 700 SRM 53 00 51 FIG 203 REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,976 hrs · 12,503 cycles

FORWARD PASSENGER CABIN MINOR SCRATCH ON FLOORBEAM AT BS 328 RBL 11. SCRATCH AND CORROSION ON FLOORBEAM AT BS 328 RBL 11 BLENDED OUT. BLEND AREA FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. FLOORBEAM REPAIRED IAW ERO 8710 AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,976 hrs · 12,503 cycles

FWD PASSENGER CABIN INTERCOSTAL AT BS 328 344 LBL 47 IS CRACKED. FWD PASSENGER CABIN INTERCOSTAL REPLACED WITH NEW PART P/N 141A5410U12, PO 122205 AT BS 328 344 LBL 47 IAW B737 700 SRM 51 40 02.

Part: FLOOR SUPPORT — SCRATCHED (FUSELAGE) · airframe 28,975 hrs · 12,503 cycles

FWD PASSENGER CABIN SCRATCHES ON FLOORBOARD SUPPORT BS 312 TO BS 328 RBL 10. FLOORBOARD SUPPORT BEAM AT BS 312 TO BS 328 RBL 10 REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT PASSENGER CABIN CORROSION ON FLOORBOARD SUPPORT BEAM. CORROSION ON FLOOR SUPPORT BEAM BLENDED OUT. AREA FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. NEW SUPPORT BEAM INSTALLED IAW B737 700 SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

CORROSION FOUND ON FLOORBEAM BS 294.5 RBL 10 52. CORROSION ON FLOORBEAM BS 294.5 RBL 10 52 BLENDED OUT. BLEND AREA FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. FLOORBEAM REPAIRED IAW B737 ERO 8715 AND EA.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,975 hrs · 12,503 cycles

FWD PASSENGER CABIN RT FWD DOOR SILL CHORD HAS MINOR CORROSION AT BS 328 RBL 62. REPLACED DAMAGED PART WITH NEW PART.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,976 hrs · 12,503 cycles

INTERCOSTAL AT BS 312 BS 328 LBL 47 IS CRACKED. CRACKED INTERCOSTAL AT BS 312 BS 328 LBL 47 REMOVED AND A NEW SERVICEABLE INTERCOSTAL WAS INSTALLED IAW B737 700 SRM 51 40 02.

Part: FLOORBEAM — SCRATCHED (FUSELAGE) · airframe 28,975 hrs · 12,503 cycles

FWD PASSENGER CABIN FLOORBEAM BS 312-328 LBL 12 SCRATCHED. FLOORBEAM AT BS 312 328 LBL 12 REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

CORROSION FOUND ON FLOORBEAM BS 312 LBL 11 TO LBL 30. CORROSION ON FLOORBEAM BS 312 LBL 11 TO LBL 30 BLENDED OUT. BLEND AREA FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. FLOORBEAM REPAIRED IAW ERO 8711 AND EA.

Part: PAN — PUNCTURED (FUSELAGE) · airframe 28,976 hrs · 12,503 cycles

AFT PASSENGER CABIN PUNCTURE IN FLOOR PAN BS 1019 LBL 16. PUNCTURE IN FLOOR PAN BS 1019 LBL 16 REPAIRED IAW ASA EA 5310 02828.

Part: FLOORBEAM — SCRATCHED (FUSELAGE) · airframe 28,975 hrs · 12,503 cycles

FWD PASSENGER CABIN BS 328 344 LBL 12 FLOORBEAM SCRATCHED. FLOORBEAM BS 328 344 LBL 12 REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,976 hrs · 12,503 cycles

FWD PASSENGER CABIN INTERCOSTAL CRACKED AT BS 312 TO BS 328 RBL 31. FWD PASSENGER CABIN CRACKED INTERCOSTAL REMOVED AND NEW SERVICEABLE INTERCOSTAL INSTALLED IAW B737 700 SRM 51 40 02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT PASSENGER CABIN INTERCOSTAL AT BS 947 BS 967 LBL 51 CORROSION FOUND. AFT PASSENGER CABIN INTERCOSTAL AT BS 947 BS 967 LBL 51 REPLACED IAW B737 700 SRM 51 40 02.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 28,976 hrs · 12,503 cycles

DENT ON AFT FACE OF 1016 BULKHEAD 0.032 INCH IN DEPTH BEYOND LIMIT IAW B737 700 SRM 53 80 08. DENT ON AFT FACE OF 1016 BULKHEAD REPAIRED IAW B737 700 SRM 53 80 08 REPAIR 1 AND EA 5310 02829.

Part: STRAP — CORRODED (CARGO BAY) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT FLOOR PANEL T-SPLICE STRAP AT BS 767+6 RBL 20 TO LBL 20 HAS CORROSION. T-SPLICE STRAP CORROSION BLENDED OUT. BLEND AREA FOUND TO BE BEYOND LIMIT. NEW REPAIR STRAP MADE IAW B737 700 SRM 53 00 53 AND 53 60 53.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,975 hrs · 12,503 cycles

AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 LBL 8.1. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDED OUT AND FOUND TO BE BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 28,976 hrs · 12,503 cycles

FWD CARGO PIT MID FLOOR PANEL BS 428 500 LBL 24 RBL 24 HAS MULTIPLE DENTS. FWD CARGO PIT MID FLOOR PANEL BS 428 500 LBL 24 RBL 24 DENT FOUND TO BE BEYOND LIMITS. FLOOR BOARD REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 00 53.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT CORROSION AROUND ANCHOR NUTS ON FLOOR SUPPORT CHANNEL AT BS 927 947 RBL 14. CORROSION AROUND ANCHOR NUTS ON FLOOR SUPPORT CHANNEL AT BS 927 947 FOUND TO BE BEYOND LIMIT. SUPPORT CHANNEL REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

FWD CARGO DOOR SILL CORRODED IN MULTIPLE SPOTS. DOOR SILL FOUND TO BE BEYOND LIMIT. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 30 01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT CORROSION AROUND ANCHOR NUTS ON SIDEWALL FLOOR SUPPORT ANGLE AT BS 947 LBL 10 RBL 21. REPLACED SUPPORT ANGLE AT BS 947 WITH A NEW ONE IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 RBL 13.84. AFT CARGO PIT FLOOR SUPPORT AT BS 767 + 6 RBL 13.84 CORROSION BLENDED OUT. BLEND AREA FOUND TO BE BEYOND LIMIT IAW B737 700 SRM 53 00 53 REF MIGS 5106709 FOR REPAIR DETAILS ITEM 7 PARTIAL WORK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,975 hrs · 12,503 cycles

AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 LBL 17.24. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDED OUT AND FOUND TO BE BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 3 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,975 hrs · 12,503 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT BS 767 + 6 RBL 8.1. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BS 767 + 6 RBL 8.1 BLEND OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT DOOR SILL AT BS 807 TO BS 847 RBL 25 CORROSION FOUND. AFT CARGO PIT DOOR SILL CORROSION BLENDED OUT. BLEND AREA FOUND TO BE BEYOND LIMIT. NEW PART INSTALLED IAW B737 700 SRM 51 40 02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,975 hrs · 12,503 cycles

AFT CARGO PIT CORROSION FOUND ON RT ZEE ANGLE AT BS 767 RBL 18. CORROSION FOUND TO BE BEYOND LIMITS IAW B737 700 SRM 53 00 53, FOR REPAIR ACTION REF CARD 5106696.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT FLOOR PANEL AT BS 767 TO 887 HAS CORROSION ON UPPER EDGES AND NUMEROUS GOUGES ON THE SIDE. AFT CARGO PIT FLOOR PANEL AT BS 767 TO 887 CORROSION BLENDED OUT. BLEND AREA FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMIT AND GOUGES FOUND TO BE BEYOND LIMITS. FLOOR PANEL REPLACED IAW B737 700 SRM 51 40 05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT TRACK BS 787 TO BS 847 + 6 RBL 14. FLOOR SUPPORT TRACK FOUND TO BE BEYOND LIMIT. REPLACED WITH MADE REPAIR PART IAW DWG 146A7501 AND SRM B737 700 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,975 hrs · 12,503 cycles

AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 LBL 3. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDED OUT AND FOUND TO BE BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,975 hrs · 12,503 cycles

AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767+6 RBL 3. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDED OUT AND FOUND BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 28,976 hrs · 12,503 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT SPLICE BS 887 LBL 10 RBL 21. CORROSION ON FLOOR SUPPORT SPLICE FOUND TO BE BEYOND LIMIT. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 00 53.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 26,530 hrs · 11,319 cycles

L1 OUTER DOOR SKIN PULLED FROM STRUCTURE FROM CONTACT WITH DOOR OPENING STRUCTURE (FRAME). REPAIRED IAW SRM 52 00 01 TO INSTALL EXTERNAL DOUBLER.

Part: OXYGEN GEN — ACTIVATED (CABIN) · airframe 24,726 hrs · 10,488 cycles

FOUND 1 EACH OXYGEN GENERATOR SPENT VIA BAND BLACK AT ROW 13DEF DURING WORKCARD INSPECTION OF OXYGEN GENERATORS TC 7803500. REMOVED SPENT GENERATOR. NEW O2 GENERATOR FAILED INSTALLATION BY INADVERTENT ACTIVATION OF PIN.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 23,800 hrs · 10,014 cycles

FWD CARGO DOOR SKIN CREASED AT STA 448. REPAIRED IAW EA 5230 01359.

Part: FLOOR PANEL — DAMAGED (FS 500)

PAE - DURING SI CHECK, FOUND FORWARD CARGO BAY AFT FLOOR PANEL FASTENER PULLING THROUGH TEMP REPAIR. REPAIRED IAW SRM 53-00-53/51-40-5. (M)

Part: SUPPORT — CORRODED (FS 727A-787)

PAE - DURING SI CHECK, FOUND CORROSION ON LEFT SIDEWALL SUPPORT PLATE AT BS 727. REPAIRED IAW SRM 53-00-53, 51-40-02. (M)

Part: STOP FITTING — CHAFED (FS 340)

PAE - DURING SI CHECK, FOUND FORWARD ENTRY DOOR AFT LOWER STOP PIN FITTING CHAFED. REPAIRED IAW EA 5210-01183. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE: DURING C-CHECK FOUND CRACKED INTERCOSTAL AT BS 328. REPAIRED IAW SRM. (K)

Part: SUPPORT — CORRODED (FS 500)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT. REPAIRED IAW SRM 53-00-53. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE: DURING C-CHECK FOUND CRACKED EBAY INTERCOSTAL AT BS 321. REPAIRED IAW SRM. (K)

Part: STOP FITTING — GOUGED (FS 324)

PAE - DURING SI CHECK, FOUND FORWARD GALLEY DOOR AFT UPPER STOP PIN IS GOUGED. REPAIRED IAW EA 5210-10082. (M)

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

PAE: DURING IS CHECK FOUND FLOOR PANEL DAMAGED. REPAIRED IAW SRM. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE: DURING IS CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727. REPAIRED IAW SRM. (K)

Part: DOOR FRAME — CHAFED (FS 312)

PAE - DURING SI CHECK, FOUND FORWARD ENTRY DOOR FORWARD FRAME CHAFED AT OB RADIUS UPPER END. REPAIRED IAW EA 5210-01181. (M)

Part: ANGLE — CORRODED (FUSLEAGE)

Z-ANGLE CORRODED. REPLACED Z-ANGLE.

Part: CARRIAGE — UNKNOWN (TE FLAP)

MODIFICATION OF FLAP CARRIAGE REQUIRED. ACCOMPLISHED EA 5750-01976.

Part: SKIN — DENTED (HORZONTAL STAB)

DENT ON LT LE HORIZONTAL STABILIZER. ACCOMPLISHED PERMANENT REPAIR.

Part: ANGLE — CORRODED (FUSELAGE)

FWD CARGO COMPARTMENT, RT ZEE ANGLE CORRODED AT STA 500C. REMOVED AND REPLACED FWD CARGO COMPARTMENT ZEE ANGLE AT STA 500C-500D.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 14,131 hrs · 5,972 cycles

AFT CARGO COMP RT ZEE ANGLE CORRODED. REMOVED AND REPLACED ZEE ANGLE IAW SRM.