N623AS

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,359 hrs · 17,209 cycles

WHILE ACCOMPLISHING TASK CARD #78233008 (EMER LIGHTS OPS CHECK) FOUND ROW 10 AND 13 ABC AND EXTERIOR BELLY LIGHTS INOP. PULLED AND TAGGED EMER CHARGER L AFT. RELAMPED ALL LIGHTS NO GOOD. REMOVED AND REPLACED L AFT BATTERY PACK. RESET BREAKER OPS CHECK GOOD. REF AMM 33 51 06 960 805.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 38,701 hrs · 16,910 cycles

PANEL 102 DOOR CUTOUT OUTBOARD SIDE ANGLE & REPAIR STRAP CHAFED. REPAIRED IAW ASA EA700 53EA 07115 & REO G14386 REV IR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,704 hrs · 16,910 cycles

MAIN CABIN R1 DOOR FLOOR SUPPORT CREASE BEAM CORRODED BS 294.5 TO BS 312 RBL 55. REMOVED AND REPLACED DOOR CHORD IAW B737 700 SRM 51 40 02 AND BOEING DWG 141A8315 REV A.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 38,705 hrs · 16,910 cycles

AFT PRESSURE BULKHEAD AT BS 1016 3EA STIFFENERS HAVE A MISDRILLED HOLE AT BL 0 LBL 7 AND LBL 14. REPAIRED AFT PRESSURE BULKHEAD AT BS 1016 3 EA STIFFENERS AT BL 0 LBL 7 AND LBL 143 IAW TIMCO REO G14405 REV B AND ASA EA 700 53EA 07153.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,705 hrs · 16,910 cycles

MAIN CABIN INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL IAW B737 700 SRM 51 40 02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,705 hrs · 16,910 cycles

AFT FUSELAGE COMPARTMENT BS 1088 RBL 28 AT APU INLET DUCT ATTACH POINT TO BULKHEAD CORRODED. REMOVED CORROSION ON STIFFENER STA 1088 RBL 28. ORIGINAL THICKNESS .071 REMOVED .009 REMAINING THICKNESS .062 FOUND TO BE OUT OF LIMITS IAW B737 700 SRM 53 80 08 UT GAUGE USE T822SM MATERIAL 10 FOR STIFFENER. REMOVED STIFFENER IAW B737 700 SRM 51 40 02. FABRICATED STIFFENER IAW B737 700 SRM 53 80 08 AND B737 700 SRM 51 70 11. ALODINED AND PRIMED STIFFENER IAW B737 700 SRM 51 20 01. INSTALLED STIFFENER STA 1088 RBL 28 IAW B737 700 SRM 53 80 08 AND B737 700 SRM 51 70 11.

Part: LATCH — LACK OF LUBE (L1 DOOR) · airframe 37,798 hrs · 16,494 cycles

L1 DOOR HOLD OPEN LATCH WILL NOT RELEASE. LUBED L1 HOLD OPEN LATCH, OPS CHECKS GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 36,675 hrs · 20,136 cycles

FLOOR SUPPORT CRACKED AT BS 540. REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,761 hrs · 14,632 cycles

MAIN CABIN FLOOR BOARD SUPPORT CRACKED. REMOVED & REPLACED FLOOR BOARD SUPPORT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,761 hrs · 14,632 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 31,254 hrs · 13,486 cycles

NUMEROUS OVERSIZE AND ELONGATED HOLES COMMON TO STA 727E 747 MODIFICATION DOUBLER. REPAIRED ELONGATED HOLES.

Part: SKIN — DENTED (CARGO DOOR) · airframe 30,177 hrs · 12,933 cycles

DENT FOUND ON FWD CARGO DOOR. INSTALLED REPAIR PER SRM 52-00-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,406 hrs · 12,540 cycles

FWD PAX CABIN INTERCOSTAL CRACKED BS 312 328 RBL 31. FWD PAX CABIN INTERCOSTAL CRACKED BS 312 328 RBL 31 REPLACED IAW B737 700 SRM 51 40 02 NEW PART P/N 141A5410U12.

Part: FLOOR SUPPORT — SCRATCHED (FUSELAGE) · airframe 29,406 hrs · 12,540 cycles

FWD PASSENGER CABIN SCRATCH ON FLOOR SUPPORT STRUCTURE BS 340 BS 344 LBL 10. FLOOR SUPPORT STRUCTURE MADE REPAIR PART (ILLEGIBLE) BS 340 BS 344 LBL 10 IAW B737 700 SRM 51 40 02 & DWG 141A5410.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

FWD CARGO DOOR SILL PLATE FAYING SURFACE ANCHOR NUT AREA CORROSION NOTED. FWD CARGO DOOR SILL PLATE REPLACED WITH NEW PART IAW B737 700 SRM 51 40 02 REFER TO PARTIAL WORK FOR DETAILS.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,406 hrs · 12,540 cycles

FWD PASSENGER CABIN CORROSION ON LATERAL INTERCOSTAL BS 270 RBL 11 LBL 10. CORROSION FOUND ON FWD PASSENGER CABIN CORROSION ON LATERAL INTERCOSTAL BS 270 RBL 11 LBL 10 WAS FOUND TO BE BEYOND LIMITS AND THEREFORE WAS REPAIRED DAW ERO 8684 AND ASA EA 5310 02820. REPLACE THE SUBJECT INTERCOSTAL WITHIN 24 MONTHS FROM 26 SEP 08.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,406 hrs · 12,540 cycles

FWD PASSENGER CABIN INTERCOSTAL CRACKED BS 328 344 LBL 46. FWD PASSENGER CABIN INTERCOSTAL REPLACED WITH NEW PART BS 328 344 LBL 46 IAW B737 700 SRM 51 40 02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

FWD CARGO PIT RT SIDE ZEE ANGLE CORRODED BETWEEN BS 500A AND BS 500D. REPLACE WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

AFT PASSENGER CABIN CORROSION ON DOOR ENTRY INNER CHORD BS 936 BS 980 RBL 54. CORRODED ENTRY DOOR INNER CHORD BETWEEN BS 936 BS 980 RBL 54 FOUND TO BE BEYOND REPAIRABLE DAMAGE LIMIT. SILL CHORD REPLACED WITH NEW PART P/N 147A8540U8 IAW SRM 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,406 hrs · 12,540 cycles

AFT PASSENGER CABIN CORROSION ON TOP OF FLOORBEAM BS 986.5 RBL 4 RBL 23. AFT PASSENGER CABIN CORROSION ON TOP OF FLOORBEAM BS 986.5 RBL 4 RBL 23 REPAIRED IAW ERO 8676 AND EA 5320 01853. PERFORM FIRST STAGE DTA INSP REQUIREMENTS WITHIN 12 MONTHS FROM 19 SEP 08. SEAMC BILL NOTIFIED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

AFT PASSENGER CABIN CORROSION ON FLOOR ANGLE BS 986.5 +7 RBL 38. AFT PASSENGER CABIN CORROSION ON FLOOR ANGLE BS 986.5 +7 RBL 38 BLENDED AND FOUND BEYOND ALLOWABLE LIMITS IAW B737 700 SRM 53 70 57. REPLACED WITH NEW PART IAW B737 700 SRM 51 40 02.

Part: SHIELD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,406 hrs · 12,540 cycles

FWD CARGO PIT RT SHIELD AT BL 21 BETWEEN BS 495 AND 500A CORRODED. RT SHIELD AT FWD CARGO PIT BL 21 BETWEEN BS 492 AND BS 500A REPLACED IAW B737 700 SRM 51 40 02 AND 53 30 15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

AFT PASSENGER CABIN CORROSION ON TOP FLOORBEAM STA 967 RBL 17 AFT PASSENGER CABIN CORROSION OF TOP FLOORBEAM STA 967 RBL 17. REPAIRED IAW CASCADE ERO 4 AND ASA 5320 01854.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

FWD CARGO PIT LT Z-ANGLE CORRODED BETWEEN BS 495 AND 500D. CORRODED FWD CARGO PIT LT Z-ANGLE CORRODED BETWEEN BS 495 AND 500D REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53.

Part: ANGLE — DAMAGED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

FWD CARGO PIT AFT BULKHEAD LOWER ANGLE BETWEEN STR 26R AND STR 26L AT BS 500D. AREA BLENDED AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. LOWER ANGLE REMOVED AND REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 20 05 & 51 40 02.

Part: TIE CLIP — MISSING (FUSELAGE) · airframe 29,406 hrs · 12,540 cycles

FWD CARGO STR 27L BS 500D TIE CLIP MISSING. FWD CARGO PIT AT BS 500B STA 27L TIE CLIP REPLACED IAW 737 700 SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,406 hrs · 12,540 cycles

CORROSION ON AFT CARGO PIT FLOORBOARD SUPPORT WEB BS 767 787 RBL 20. AFT CARGO PIT FLOORBOARD SUPPORT WEB BS 767 787 RBL 20 REPLACED WITH MADE REPAIR PART IAW 737 700 SRM 51 40 02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,406 hrs · 12,540 cycles

CORROSION ON AFT CARGO TIE DOWN TRACK BS 787 BS 847 RBL 14. CORRODED AFT CARGO TIE DOWN TRACK BS 787 BS 847 RBL 14 REPLACED WITH NEW TIE DOWN TRACK IAW B737 700 DWG 146A7501 MADE FROM BAC1520 1397.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,406 hrs · 12,540 cycles

AFT CARGO Z-CHANNEL BS 727E +10 TO BS 847 CORRODED LBL 20 CORROSION ON Z CHANNEL BS 727E +10 TO BS 847 CORRODED LBL 20 IN AFT CARGO PIT BLENDED AND FOUND TO BE BEYOND LIMITS. REPLACED WITH MADE REPAIR PART IAW 737 700 SRM 53 00 53 REPAIR 6.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

AFT CARGO DOOR SILL PLATE FAYING SURFACE CORRODED AROUND ANCHOR NUTS. REPLACED SILL WITH NEW PART IAW B737 700 SRM 51 40 02 AND 51 40 05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 1 · airframe 29,406 hrs · 12,540 cycles

CORROSION ON Z-CHANNEL RT BS 727C BS 767 RBL 20 AFT CARGO PIT. CORRODED ON ZEE CHANNEL AT RT BL 20 AFT CARGO PIT BETWEEN BS 727 + 4 BS 847 REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 20 05.

Part: SKIN — DENTED (BS 365-420) · airframe 24,156 hrs · 9,985 cycles

RIGHT SIDE OF FUSELAGE FWD OF FWD CARGO DOOR HAS A DENT ON LOWER CENTER. BS 365 REPAIRED IAW EA 53 30 02188.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 24,156 hrs · 9,985 cycles

FLOORBEAM UPPER TEE IS CORRODED AT BS 986 REPAIRED IAW EA 5310 02703.

Part: FLOOR PANEL — GOUGED (BS 976-986) · airframe 24,156 hrs · 9,985 cycles

CABIN FLOOR PANEL 241AAF IS GOUGED AT FWD LEFT CORNER REPAIRED IAW EA5320 100.

Part: HINGE — DAMAGED (APU DOOR) · airframe 24,156 hrs · 9,985 cycles

APU ACCESS DOOR HINGE AREA DAMAGED REPAIRED IAW SRM 53-80-01.

Part: INTERCOSTAL — CORRODED (BS 967) · corrosion level 2 · airframe 24,156 hrs · 9,985 cycles

FLOORBOARD SUPPORT INTERCOSTAL IS CORRODED AT BS 967 REPAIRED IAW SRM 51-40-02.

Part: ATTACH FITTING — LOOSE (BS 243-260) · airframe 24,156 hrs · 9,985 cycles

NOSE LANDING GEAR RETRACT ACTUATOR UPPER ATTACH LUG BEARING IS LOOSE AND MIGRATING REPAIRED IAW SRM 51-40-02.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 24,156 hrs · 9,985 cycles

CABIN FLOORBOARD IS DAMAGED AT 951 REPAIRED IAW SRM 53-00-50.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 24,156 hrs · 9,985 cycles

CABIN FLOORBOARD HAS DAMAGE AT 927 REPAIRED IAW SRM 53-00-50 REPAIR 9.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 24,156 hrs · 9,985 cycles

CABIN FLOORBOARD AT 967 DAMAGED REPAIRED IAW SRM 53-00-50 REPAIR 2.

Part: SEAT TRACK — CORRODED (FS 773)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TRACK AT BS 773. REPAIRED IAW SRM 53-00-53. (M)

Part: FLOOR SUPPORT — CORRODED (FS 773)

PAE - DURING CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M)

Part: FLOOR SUPPORT — CORRODED (FS 773)

PAE - DURING CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IW EA 5310-02493. (M)

Part: SKIN — CRACKED (FS 233-228)

PAE - DURING CHECK, FOUND EXT POWER DOOR CUT OUT CRACKED. REPAIRED IAW EA 5330-01996. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT CORRODED. REPAIRED IAW SRM. (K)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE: DURING C-CHECK FOUND STRINGER CLIP AT BS 847 CRACKED ON OB LEG. REPAIRED IAW SRM. (K)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

PAE: DURING C-CHECK FOUND FOUND AFT CARGO BAY FLOOR PANEL NR 2 GOUGED AND CRACKED. REPAIRED IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FS 773)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M)

Part: FLOOR PANEL — GOUGED (AFT CARGO BAY)

PAE: DURING C-CHECK FOUND AFT CARGO BAY NR 3 FLOOR PANEL GOUGED AND DENTED. REPAIRED IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FS 773)

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

Part: FLOOR SUPPORT — CORRODED (FS 773)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M)

Part: FLOOR SUPPORT — CORRODED (FS 773)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW EA 5310-02493. (M)

Part: FLOOR PANEL — DENTED (FUSELAGE)

PAE: NR 3 FLOOR PANEL OF FWD CARGO PIT HAS NUMEROUS DENTS. REMOVED AND FABRICATED NEW IAW SRM. (K)

Part: SKIN — DAMAGED (FUSELAGE)

OKC - TOW BAR SNAPPED CAUSING RT FUSELAGE DAMAGE FORWARD OF FORWARD CARGO DOOR AT STA 375 TO 410 BETWEEN STR 18R AND 20R. REPAIR IAW EA 5330-01838.

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FRAME AND ANGLE AT FR28A ON THE RT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FRAME AND ANGLE AT FR 28A ON THE RT SIDE IAW WITH SRM 51-25-01.