N321DL

Part: SKIN — CRACKED (BS 480) · airframe 79,960 hrs · 63,034 cycles

FUSELAGE SKIN CRACKED AT STRINGER 16R JUST AFT OF BS 480. A DOUBLER AND TRIPLER WAS INSTALLED IAW SRM, 53-30-03, REPAIR 48, DETAIL VII.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,828 hrs · 62,911 cycles

3 INCH LONG CRACK FOUND IN FUSELAGE SKIN DIRECTLY BELOW S23R AT BS 344. CAT B REPAIR INSTALLED IAW SRM 53-30-3, FIGURE 48, DETAIL XVIII.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,120 hrs · 62,264 cycles

SKIN CRACK FOUND ON RIGHT SIDE FUSELAGE S16R AND BS445 (VERIFIED WITH HFEC). DAMAGE REMOVED, DOUBLER INSTALLED REF SRM 53-30-3, FIG 48, REV SEP 2016. DETAIL XI AND III, PROCEDURE VII.

Part: ENGINE — FAILED (NR 2) · airframe 77,718 hrs · 60,962 cycles

NR 2 ENGINE FAILED AT 2000 FEET ON TAKEOFF. MI AT 1705 FEET DURING CLIMB, LOUD NOISE FROM NR 2 ENGINE, NO EPR, SMOKE IN COCKPIT, AND ENGINE VIBRATION. NR 2 ENGINE HAD A FAILURE OF MULTIPLE STAGES OF THE TURBINE SECTION. THE ENGINE AND THRUST REVERSER WERE REMOVED AND REPLACED. THE ENGINE SEIZURE PHASE 2 CONDITIONAL INSPECTION WAS PERFORMED IAW AMM 05-51-61 AND THE PARTS DEPARTS AIRPLANE CONDITIONAL INSPECTION WAS ACCOMPLISHED IAW AMM 05-51-59.

Part: FLOORBEAM — CORRODED (BS 827) · corrosion level 2 · airframe 76,881 hrs · 60,175 cycles

CORROSION ON TOP SURFACE OF FLOORBEAM AT BS 827 LBL 49 - 56. CORROSION BLENDED OUT OF LIMITS IAW SRM 53-10-1, FIG 1, REV 113. REPAIRED THE FLOORBEAM IAW DWG R23093.1-053-023-001, REV NC.

Part: INTERCOSTAL — CRACKED (BS 277) · airframe 76,881 hrs · 60,175 cycles

CRACK IN RADIUS OF INTERCOSTAL BS 277 STRINGER 10R FORWARD OF R1 DOOR. REPLACED INTERCOSTAL ANGLE IAW SERVICE BULLETIN-737-53A1241 REV 1.

Part: FLAP TRACK — DAMAGED (RT WING TE FLAP) · corrosion level 2 · airframe 76,881 hrs · 60,175 cycles

RIGHT INBOARD FLAP OUTBOARD TRACK REPAIR BUSHING CAD PLATING DETERIORATED. FLAP TRACK REPLACED IAW AMM 27-51-161, REV 12.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 76,881 hrs · 60,175 cycles

CRACKED STRINGER CLIP BS 663, STRINGER 10R, REPLACED THE STRINGER CLIP IAW SRM 51-30-2, REV 113.

Part: ANGLE — CRACKED (BS 663) · airframe 76,881 hrs · 60,175 cycles

ANGLE CRACKED AT BS 663, LBL 24.82. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW DWG PL65-45410 REV DD, BSB 737-57A1296, SRM D6-15565 REV 113, AND 51-30-02.

Part: BULKHEAD WEB — CRACKED (BS 1016) · airframe 76,881 hrs · 60,175 cycles

CRACKED RIVETS ON BS 1016 BULKHEAD WEB BETWEEN STRINGERS 5 - 7L. REPAIRED IAW SRM 113 53-10-4, FIGURE 15.

Part: FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 76,881 hrs · 60,175 cycles

RIGHT OUTBOARD FLAP, NR 7 CARRIAGE SUPPORT FITTING CORRODED ON THRUST BEARING SURFACE (IN MID FLAP). REPLACED WITH REPAIRED ASSY.

Part: TEE FITTING — CRACKED (BS 470) · airframe 76,881 hrs · 60,175 cycles

CRACKED TEE ON FORWARD CARGO DOOR INTERNAL STRUCTURE AT BS 470. THE TEE WAS REPLACED IAW DWG 65-46921 REV M, AND SRM D6-15565 REV 113 51-30-02.

Part: INTERCOSTAL — CRACKED (BS 294) · airframe 76,881 hrs · 60,175 cycles

CRACK IN RADIUS OF INTERCOSTAL AT BS 294.5, STRINGER 14R. REPLACED THE INTERCOSTAL IAW SERVICE BULLETIN 737-53A1241 REV 1.

Part: SPINDLE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 76,881 hrs · 60,175 cycles

LEFT OUTBOARD FLAP, NR 1 CARRIAGE SPINDLE CORRODED. THE CARRIAGE WAS REPLACED IAW MM 27-51-81, REV 123.

Part: FLAP TRACK — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 76,881 hrs · 60,175 cycles

LEFT OUTBOARD FLAP NR 1 TRACK CORRODED. REPLACED THE FLAP TRACK IAW AMM 27-51-151, REV 123.

Part: FRAME — CRACKED (BS 787) · airframe 76,881 hrs · 60,175 cycles

CRACKED FRAME AT BS 787, RBL42, STRINGER 13R. REPAIRED IAW SR 4-3658265861, & 8100-9.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 76,881 hrs · 60,175 cycles

CRACK FOUND IN RIGHT AFT SUPPORT FITTING FOR MAIN LANDING GEAR AT RSS 224. REPLACED THE SUPPORT FITTING IAW SERVICE BULLETIN 737-57-1216, REV 2, & SR 4-3648350626, AND 8100-9.

Part: STRINGER CLIP — CRACKED (BS 967) · airframe 76,881 hrs · 60,175 cycles

CRACKED STRINGER CLIP AT BS 967, STRINGER 22L. REPLACED IAW SRM 51-30-2 REV 113 AND DWG 65-46563 REV -.

Part: ATTACH FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 76,881 hrs · 60,175 cycles

RIGHT OUTBOARD FLAP, NR 8 TRACK FORWARD ATTACH FITTING (ON WING) HAS EVIDENCE OF CORROSION BETWEEN TRACK ATTACH BUSHINGS. REPLACED THE FWD ATTACH FITTING IAW BAC5047, AMM 20-50-11 REV 123, & DWG 65-45455 REV E.

Part: BULKHEAD WEB — CRACKED (BS 1016) · airframe 76,881 hrs · 60,175 cycles

ONE CRACK ON BS 1016 BULKHEAD WEB AT STRINGER 15R. REPAIREDTHE BULKHEAD WEB IAW SR 4-3633491853, & 8100-9.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 76,881 hrs · 60,175 cycles

CRACKED STRINGER CLIP BS 663, STRINGER 10L, WL 256. REPLACED THE STRINGER CLIP IAW SRM 51-30-2 REV 113, & DWG 65-46541 REV H.

Part: STRINGER SPLICE — CORRODED (BS 887-907) · airframe 72,772 hrs · 56,531 cycles

DAMAGE FOUND ON STRINGER SPLICE BS907, STR20L IN AFT PIT. DAMAGED STRINGER SPLICE AT BS907, STR20L IN AFT PIT REPLACED IAW SRM 51-10-01, PARA 7, REV 108. INSTALLED IAW SRM 51-30-02, REV 108. CORRODED SECTION OF STRINGER BETWEEN FS887-907 STR20L REPAIRED IAW SRM 53-10-03, FIG 1, REV 108 & INSTALLED IAW SRM 51-30-02, REV 108.

Part: STRINGER — DAMAGED (BS 1016) · airframe 72,772 hrs · 56,531 cycles

AFT PIT AT STR 21R DAMAGED JUST FWD OF BS1016. AFT CARGO PIT STR 21R JUST FORWARD OF STA 1016. REPLACED WITH FABRICATED PART IAW SRM 53-10-2, FIG 9, ITEM 14, REV 108. INSTALLED IAW SRM 51-30-2, REV 108, REF MCO3008, W/O 1358115.

Part: FLOORBEAM — CORRODED (BS 887) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON FLOORBEAM MAIN CABIN BS887 BETWEEN LBL25-45 AND 21.5L. CORROSION AT STA 887, LBL 21.5 TO LBL 45 ON FLOORBEAM BLENDED, MEASURED AND FOUND TO BE OUT OF LIMITS. INSERTED REPLACEMENT BEAM CAP SECTION IAW SRM R108, 53-10-9, FIG 3, REF MCO 3008, WO 1348637.

Part: FRAME — CRACKED (BS 747) · airframe 72,772 hrs · 56,531 cycles

FRAME CRACKED FROM RIVET RUNNING ACROSS RADIUS, APPROXIMATELY 1" LONG AT BS 747, WL 235, BL70L. REPAIRED CRACKED FRAME FROM RIVET RUNNING ACROSS RADIUS AT STA 747, WL 235, BL 70L IAW SRM 53-10-4, FIG 1, REV 108, REF MCO3008, W/O 1349146.

Part: FRAME — CORRODED (BS 277) · airframe 72,772 hrs · 56,531 cycles

NOSE WHEEL WELL CORROSION ON FRAME AT BS 277 WHERE FRAME MEETS LOWER CHORD ON RT SIDE. REPAIRED FRAME IN NOSE WHEEL WELL AT STA 277 RT SIDE, REPAIRED IAW DWG R23093, 1-053-012-001, REV NC AND SRM 51-30-02, REV 108 AND DWG 65-45819, SHEET 6, REV T, REFERENCE MCO3008 W/O 1355813.

Part: STRINGER — CORRODED (BS 727-727A) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON STR20L AT BS727-727A IN AFT PIT. CORRODED STR20L AT BS727-727A IN AFT PIT REPAIRED IAW SRM, REV 108, SECTION 53-10-3, FIG 1.

Part: FLOORBEAM — CORRODED (BS 927) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON FLOORBEAM BS 927, LBL 36-42. CORROSION ON FLOORBEAM AT STA 927 AT LBL 25 TO LBL 45 BLENDED, MEASURED AND FOUND TO BE BEYOND LIMITS. REPAIRED IAW SRM R108, 53-10-9, FIG 3. REF MCO 3008, WO 1349194.

Part: STRINGER SPLICE — CRACKED (BS 360) · airframe 72,772 hrs · 56,531 cycles

CRACK IN STR SPLICE AT BS360 STR 15L. STR SPLICE AT STA 360, STR 15L REPLACED IAW SRM 51-10-01, PARA 7 AND INSTALLED IAW SRM 51-30-02, REV 108. REF MCO3008, W/O 1349110.

Part: FRAME — CRACKED (BS 793) · airframe 72,772 hrs · 56,531 cycles

CRACKED FWD FRAME OF AFT PIT DOOR OPENING BS793 AT LWR STOP NR 1. REMOVED CRACKED FRAME AT BS793, INSTALLED NEW FRAME PN 65-47959-78, INSTALLED ALL AFT CARGO PIT DOOR IAW AMM 52-31-00, PG 401. INSTALLED ALL DOOR STOPS PERFORMED ADJUSTMENT AND FIT CLEARANCE CHECKS. PERFORMED DOOR WARNING SYSTEM ADJUSTMENT TEST IAW AMM 52-71-00, PG 501. REF MCO 3008, W/O 1347791.

Part: FLOORBEAM — CORRODED (BS 928) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON UPPER CAP OF FLOORBEAM BS 928 BETWEEN RBL 25-RBL 45. CORROSION ON FLOORBEAM AT STA 928 RBL 25-RBL 45. BLENDED, MEASURED AND FOUND TO BE BEYOND LIMITS. REPAIRED TRACK IAW SRM R108, 53-10-5, FIG 2 AND AEI DWG AE4943, REV A, REF MCO 3008, WO 1349213.

Part: FRAME — CRACKED (BS 277) · airframe 72,772 hrs · 56,531 cycles

CRACK IN FRAME, BS277 AT STR16L. REPAIR CRACKED FRAME AT BS277, STR16L IAW SRM 53-10-4, FIG 4 REPAIR 2, REV 108.

Part: FRAME — DAMAGED (BS 747) · airframe 72,772 hrs · 56,531 cycles

BELTFRAME DAMAGED AT BS 747 BETWEEN STR 16R-STR 17R. PHYSICAL DAMAGE NOTED TO BELT FRAME INBD CHORD AT BS 747, STR 16-17R. REPAIRED & INSTALLED IAW SRM 51-30-02. 8110-3, DWG R23093.1-053-011-001, REV NC, DER REPAIR. REF MCO 3008, WO 1354926.

Part: STRINGER CLIP — CRACKED (BS 420) · airframe 72,772 hrs · 56,531 cycles

CRACKED STRINGER CLIP AT BS 420, STR 4R. CRACK STRINGER CLIP AT STA 420, STR 4R. REPLACED IAW SRM 51-20-1, FIG 7 AND SRM 51-30-02. MATERIAL ID IAW SRM 51-10-3, REV 108. REFERENCE MCO3008 W/O 1349111.

Part: FRAME — CRACKED (BS 500) · airframe 72,772 hrs · 56,531 cycles

FWD PIT BELTFRAME CRACKED AT BS 500, LBL 1 BETWEEN STR 28L & STR 28R. REPAIRED FWD PIT BELT FRAME AT STA 500, LBL 1 BETWEEN STR 28R - STR 28L WITH NESTED ANGLE REPAIR IAW DWG R23093.1-053-013-001, REV 1 AND DER 8110. REF MCO 3008, WO 1356529

Part: SKIN — CRACKED (BS 302-346) · airframe 72,772 hrs · 56,531 cycles

CRACK IN INTERIOR ACFT SKIN AT LOWER AFT CORNER OF FWD AIRSTAIR DOOR CUTOUT. CRACK WAS REPAIRED IAW SB 53-1058-R4 WHICH CALLS UP DWG 65C20843. AN ALLOWANCE TO TRIM BACK THE MAIN CARGO DOOR DOUBLER WAS RECEIVED FROM SIE UNDER R23093.1-053-016-001, REV NC, REF MCO 3008, WO 1356811.

Part: FLOORBEAM — CORRODED (BS 480) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON FLOORBEAM BS 480 FLOOR BL 50R-02R. CORRODED FLOORBEAM AT STA 480, RBL 50-RBL62. REPAIRED IAW SRM 53-10-09, FIG 1, REV 108. WITH NESTED ANGLES. INSTALLED IAW SRM 51-30-02, REV 108. REF MCO3008 W/O 1349303.

Part: STRUCTURE — CRACKED (SERVICE DOOR) · airframe 72,772 hrs · 56,531 cycles

R1 DOOR CRACKED IN LWR AFT CORNER. CRACKED SPLICE IN R1 DOOR REMOVED. INSTALLED NEW SPLICE ON R1 DOOR IN LWR AFT CORNER IAW SRM 51-30-02, REV 108.

Part: STRAP — CRACKED (BS 328) · airframe 72,772 hrs · 56,531 cycles

STABILIZER STRAP AT BS 328, RBL 30 CRACKED, E & E COMPARTMENT. REPAIRED CRACKED STABILZER STRAP AT STA 328, RBL 30 IAW SRM 53-10-09, FIG 4, REV 108. REPAIRED IAW SRM 51-30-02, REV 108, REFERENCE MCO3008, W/O 1354407.

Part: WEB — CORRODED (BS 907-917) · airframe 72,772 hrs · 56,531 cycles

CORROSION AROUND UNDER SIDE OF FASTENER POINTS ALONG DUST SILL AT BS910-944, LBL57-61. REPLACED WEB AT BS 9007-917, LBL 57-66 WITH MADE REPAIR PART REF: DWG 65-52878, SHEET 2, REV C AND INSTALLED IAW SRM 51-30-2, REV 108.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,772 hrs · 56,531 cycles

CRACK IN SKIN AT FWD UPPER CORNER OF L1 DOOR OPENING. REPAIRED CRACK IN SKIN AT FWD UPPER CORNER OF L1 DOOR OPENING IAW SB 737-53A1163, REV 1, REPAIR 65C36941-5 & SR 3-3118154710, REF: 8110-9 ID 201501300008-0002D1.

Part: WEB — CRACKED (BS 710) · airframe 72,772 hrs · 56,531 cycles

SUSPECTED CRACK ON FLOOR WEB BS710, RBL24 IN MAIN CABIN. REPAIRED FLOOR WEB AT BS710, RBL24 IN MAIN CABIN IAW SB-37-57-1296, FIG 22, FIG 16, REV 1, SEP 26 2012.

Part: FLOORBEAM — CORRODED (BS 887) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON UNDER SIDE & TOP OF FLOORBEAM UPPER CAP AT BS 887, RBL 65-RBL 45. REPAIRED CORRODED FLOOR BEAM CAP AT BS 887, BL45, RIGHT TO BL 65, RIGHT. CUTOUT CORRODED AREA UNDER ANCHOR NUT AND INSTALLED NESTED ANGLE REPAIR. REF MCO 3008, WO 1349316.

Part: NONE — NONE (NONE) · airframe 72,772 hrs · 56,531 cycles

REPLACE PATCHES ON RT STABILIZER L/E WITH FLUSH REPAIR. REPLACED PATCH WITH FLUSH FIT REPAIR, IAW ARM 55-10-3, FIG 2, REV 108. REFERENCE MCO 3008, W/O 1349438.

Part: STRINGER — DAMAGED (BS 1016) · airframe 72,772 hrs · 56,531 cycles

AFT PIT STR 20R DAMAGED JUST FWD OF BS1016. REPAIRED AFT CARGO PIT, STR 20R JUST FORWARD OF STA 1016 IAW SRM 53-10-3, FIG 1, REV 108, SRM 51-30-2, REV 108. REF MCO3008, W/O 1358114.

Part: FRAME — CRACKED (BS 277) · airframe 72,772 hrs · 56,531 cycles

CRACKED BELT FRAME WEB AT BS277 STR 16R. CRACKED BELT FRAME WEB AT STA 277, STR 16R. REPAIRED IAW SERVICE REQUEST 3-3118662701, DOUBLER REPAIR, AND RADIUS FILLER FABRICATED IAW SRM 53-00-07, REPAIR 15. ACCEPTABLE BY FAA 8100.9 REF MCO3008, W/O 1348553.

Part: FLOORBEAM — CRACKED (BS 718) · airframe 72,772 hrs · 56,531 cycles

FLOORBEAM WEB BS 718, BL 0 FOUND CRACKED 4" AFT OF SB REPAIR. REPLACED CRACKED FLOORBEAM WEB IAW DWG 65-45410, REV H AT STA 718, BL 0, 4" AFT OF SB REPAIR. REFERENCE MCO 3008, W/O 1350149.

Part: FRAME — CRACKED (BS 767) · airframe 72,772 hrs · 56,531 cycles

AFT PIT INT BS 767, WL 152, LBL 1 FRAME CRACKED. FRAME REPLACED AND INSTALLED IAW SRM 51-30-2, REV 108. AND DWG 65-46549, REV D, REF MCO 3008, WO 1346548.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 72,772 hrs · 56,531 cycles

L1 DOOR FOUND CRACKED & PREVIOUSLY REPAIRED, VERIFIED FOR CORRECT REPAIR. REPAIRED CRACK ON L1 DOOR WITH MADE REPAIR PART IAW SRM 51-40-03, FIG 1.

Part: FRAME — DAMAGED (BS 1016) · airframe 72,772 hrs · 56,531 cycles

HOLE DAMAGE IN BS 1016 FWD OTBD FLANGE BETWEEN STR 20R-21R. REMOVED OLD AFT SKIN REPAIR, DISCOVERED HOLE DAMAGE IN FLANGES AT STA 1009-STA 1016 FORWARD OTBD FLANGES BETWEEN STR 20R-21R. REPAIRED IAW BAC 8100.9, REF ID 201502090005-0003D1 REF MCO 3008, WO 1358116.

Part: SHEAR TIE — CRACKED (BS 927) · airframe 72,772 hrs · 56,531 cycles

AFT PIT INT LBL2, WL148 FRAME SHEAR TIE CRACKED AT RIVET HOLE LOCATION. AFT PIT, INT BS927. LBL2, WL148. FRAME SHEAR TIE CRACKED AT RIVET HOLE LOCATION. REPAIRED CRACKED SHEAR TIE FRAME AT CRACKED RIVET HOLE IN AFT PIT INT BS927, LBL2, WL148 IAW SRM 53-10-4 FIG. 6, REV 108. ON KEL WO 1349030.

Part: STRINGER SPLICE — DAMAGED (BS 907) · airframe 72,772 hrs · 56,531 cycles

DAMAGE FOUND ON STRINGER SPLICE BS907, STR19L IN AFT PIT. REPLACED DAMAGED STRINGER SPLICE AT STA 907 STR 19L IAW DWG 65-45777, REV G AND INSTALLED NEW STRINGER SPLICE IAW SRM 51-30-02, REV 108. REF MCO3008, W/O 1347111.

Part: KEELBEAM — CORRODED (BS 727B) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON KEEL BEAM AT BS 727B R ON INSIDE OF AFT PIT, EXFOLIATING AND BULGING ON SKIN AFT OF KEEL SPLICE AT BS727B. REPAIRED KEEL BEAM STA 727A STR27R ON INSIDE OF AFT PIT, AFT OF KEEL SPLICE AT STA727A STR27R IAW TASS INC, DOC 121058-R022, REV 00.

Part: FLOORBEAM — CORRODED (BS 727B) · airframe 72,772 hrs · 56,531 cycles

CORROSION ON FLOORBEAM AT BS 727B BETWEEN BL 0-LBL 25 MAIN CABIN FLOOR AND BS 727B LBL 25-45 AND BS 727B LBL 45-65. CORROSION ON FLOORBEAM AT STA 727B, BL 0 - BL 65 BLENDED AND FOUND TO BE BEYOND LIMITS. REPAIRED WITH NESTED ANGLES IAW SRM R108, 53-10-9, FIG 7. REF MCO 3008, WO 1349207.

Part: STRUCTURE — CRACKED (L2 DOOR) · airframe 72,772 hrs · 56,531 cycles

L2 DOOR CRACKED AT TOP FWD CORNER. L2 DOOR REPAIRED AT TOP FWD CORNER IAW SRM 51-40-3, FIG 1, REV 108.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 72,772 hrs · 56,531 cycles

CRACKED LIGHTNING HOLE ON THE INSIDE SKIN ON THE FWD PIT CARGO DOOR AT BS450. BLENDED EDGE DAMAGE AT LIGHTNING HOLE ON THE INSIDE SKIN FWD LOWER CARGO DOOR AT STA 450. REMOVED AND FOUND TO BE BEYOND LIMITS IAW SRM 53-10-01, FIG 1, DETAIL 2, REV 108. REPAIRED IAW SRM R108, 51-40-02, FIG 1. NOTE: NO DTE REQUIRED. FLAGNOTE B FCBS. REF MCO 3008, WO 1348456.

Part: SLEEVE — LEAKING (OIL FILTER) · airframe 72,418 hrs · 56,209 cycles

NR 1 ENGINE SHUTDOWN DOWN DUE TO LOSS OF OIL PRESSURE. ENGINE MAIN OIL FILTER HOUSING ON GEARBOX SLEEVE BORE REPAIR LEAKING AT MATING SURFACES. REMOVED REPAIR SLEEVE, CLEANED AREA AND REINSTALLED SLEEVE WET WITH ADHESIVE. REF: EM 72-61-01, REPAIR 43, PARA 4. RAN ENGINE TO 3000 LBS FUEL FLOW FOR 3 MINUTES, ZERO DROPS NOTED. PERFORMED CONDITIONAL INSPECTION FOR ENGINE WINDMILLING, REF: EM 72-00-00, ADJ TEST 01, PG 532, 1, A, NO DEFECTS NOTED.

Part: SKIN — CRACKED (BS 727B) · airframe 71,919 hrs · 55,728 cycles

TWO INCH CRACK IN FUSELAGE CHEM MILLED POCKET AT STRINGER S18R, BS 727B.

Part: SKIN — CRACKED (BS 760) · airframe 71,646 hrs · 55,458 cycles

FUSELAGE SKIN CRACKED ON LT SIDE AFT OF WING ROOT STRINGER 18L, BS 760. REPAIRED IAW SRM 53-30-3, FIG. 48, DETAIL VII.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 71,646 hrs · 55,458 cycles

AFT CARGO DOOR CRACKED AT EXTERNAL DOOR HANDLE CUT-OUT, AFT UPPER SIDE OF CUT-OUT. REPAIRED DOOR IAW SRM 52-00-3, FIG 6, CAT B REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,614 hrs · 54,474 cycles

CRACK IN FUSELAGE SKIN AT BS 530, S16R. INSTALLED REPAIR IAW SRM 5-30-3, FIG 48, DETAIL VII.

Part: SKIN — CRACKED (BS 937) · airframe 70,284 hrs · 54,174 cycles

CRACK IN FUSELAGE SKIN AT BS 937, STRINGER 24R. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XIX, SHEET 46.

Part: SKIN — CRACKED (BS 920) · airframe 70,384 hrs · 54,174 cycles

CRACK IN FUSELAGE SKIN AT BS 920, STRINGER 25R ABOVE LAP SEAM. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XIX, SHEET 46.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 69,137 hrs · 53,085 cycles

ABORTED TAKEOFF DUE TO INTERMITTENT EGT NR 1 GAUGE. REMOVED AND REPLACED INDICATOR.

Part: ENGINE — FAILED (NR 1) · airframe 69,098 hrs · 53,047 cycles

NR 1 ENGINE FAILURE IN FLIGHT, ENGINE SHUT DOWN. REMOVED AND REPLACED ENGINE DUE TO TURBINE FAILURE.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION UNDER ANTENNAS ON KEEL BEAM PANEL AT BS 578 - BS 616 BETWEEN RIGHT AND LEFT AIR CONDITIONING EQUIPMENT BAYS. CORROSION UNDER ANTENNA ON KEEL BEAM PANEL AT STA 578616 FOUND TO BE BEYOND LIMITS, PANEL REPLACED WITH MADE REPAIR PART, MATERIAL IDENTIFIED PER B737200 SRM REV 105 CHAPTER 53302 FIG 3, PANEL INSTALLED IAW CHAPTER 51302.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACK IN LOWER CHORD ORIGINATING FROM AFT HOLE AT LBL 24.82 BS 663. CRACK IN LOWER CHORD ORIGINATING FROM AFT HOLE AT LBL 24.82 STA 663. REPAIRED IAW BOEING MESSAGE KFCNAC1300105B AND B737 SRM 513002 REV 105 AND BOEING MESSAGE KFCNAC13000107B.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACKED INTERCOSTAL SUPPORT ANGLE AT BS 348 S15L LOWER SIDE UNDERNEATH. REPAIRED CRACKED INTERCOSTAL SUPPORT ANGLE STA 348 LEFT STR 15 LWR SIDE IAW BOEING 737200 SRM 511001 REV 105 & 737200 SRM 513002 REV 105 AND WITH BOEING SERVICE BULLETIN 73753A1240.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON ANGLE THAT ATTACHES BELT FRAME BS 986.5 TO BELLY SKIN BETWEEN STRINGER 24R AND 25R IN EQUIPMENT BAY OF AFT CARGO PIT. CORROSION ON ANGLE THAT ATTACHES BELTFRAME STA 986.5 TO BELLY SKIN BETWEEN STRINGER 24R AND 25R IN EQUIPMENT BAY OF AFT CARGO PIT BEYOND LIMITS. NEW ANGLE INSTALLED IAW BOEING DRAWING 6546564 REV AB.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

LIGHT CORROSION IN SEAT TRACK AT VARIOUS LOCATIONS FROM BS 927 - BS 986.5, LBL 40. CORROSION ON SEAT TRACK STA 927-986.5 BL 40 LEFT FOUND BEYOND LIMITS, NEW SEAT TRACK INSTALLED IAW B737 SRM REV 105 51-10-1 PARA 7 AND 51-30-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON SEAT TRACK FLANGE AND TRACK AT SEVERAL LOCATIONS BS 927 - BS 986.5 RBL 40. CORROSION ON SEAT TRACK FLANGE STA 927986.5 RIGHT BL 40 RIGHT IS BEYOND LIMITS. NEW SEAT TRACK INSTALLED, MTRL IDENTIFIED IAW B737 SRM CHPT 53102 REV 105. NEW SEAT TRACK INSTALLED IAW B737 SRM CHPT 51101 AND 51301 REV 105.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACK IN FUSELAGE SKIN AT BS 767, S18L. REPAIRED CRACK IN FUSELAGE SKIN IAW BOEING SB 737531065 FIG 54 SHTS 15 REV 2 STA 767, STR 18L. PREPPED AND RENEWED PAINT ON FUSELAGE AT STA 767, STR 18L IAW BOEING 737200 MM 5121171 REV 119.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

STRINGER SPLICE HAS CORROSION ON IT BETWEEN BS 907 - BS 927 S19R. REPLACED STRINGER SPLICE BETWEEN STA 907-927 STR 19 IAW B737 SRM REV 105 CHAPTER 51-10-1 PARAGRAPH 7 AND CHAPTER 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON S27L STRINGER FITTING AT BS 1016 IN AFT CARGO PIT EQUIPMENT BAY. REMOVED & RE-INSTALLED NEW STRINGER FITTING AT STA 1016 STR 27L IN AFT CARGO PIT EQUIPMENT BAY IAW B737200 SRM REV 105 51101 & WITH B737200 SRM REV 105 51304. ALSO BOEING ENGINEERING DOCUMENT DRAWING 6549574 REV AR & FASTENERS INSTALLED IAW BOEING 737200 SRM REV 105 513002.

Part: SILL — CORRODED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

LIGHT CORROSION ON LOWER SILL WEB AFT CARGO PIT. CORRODED AFT CARGO PIT LOWER SILL WEB REMOVED AND REPLACED AS PER B737200 SRM 51101 & 51302 REVISION 105.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON TOP FLANGE OF FLOORBEAM BS 947 RIGHT RBL 48 AT FLOORBOARD FASTENER HOLE. CORROSION ON TOP FLANGE OF FLOORBEAM STA 947 RIGHT BL 48 RIGHT AT FLOORBOARD FASTENER HOLE IS BEYOND LIMITS. FLOORBEAM REPAIRED IAW B737 DWG 5310D1577 REV IR.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACKED SUPPORT ANGLE AT UPPER HINGE INTERCOSTAL FOR RIGHT FORWARD SERVICE DOOR BS 298. REMOVED & RE-INSTALLED NEW SUPPORT ANGLE AT UPPER HINGE INTERCOSTAL FOR RT SERVICE DOOR STA 298 IAW BOEING 737200 SRM 51101 REV 105 & IAW BOEING 737200 SRM 5130 REV 105 & BOEING ENGINEERING DRAWING 6545804 REV AG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACKED UPPER FLANGE OF INTERCOSTAL BS 348 - BS 360 LBL10. REPLACED UPPER FLANGE OF INTERCOSTAL AT STA 348-360 LBL 10 IAW B737200 SRM 511001 PARA 7 REV 105, 513002 REV 105.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACK FOUND ON C1 ORIFICE STOP FRAME LOWER INBOARD HOLE AT BS 420 BETWEEN S20 - S21R. CRACK ON C1 ORFICE STOP FRAME LOWER I/B HOLE AT STA 420 BETWEEN STR 2021R REPAIRED IAW B737 SRM REV 105 51403 FIG 1 AND 53102 FIG 3 AND SB 73753A1228/ FASTENERS INSTALLED IAW B737 SRM 513002 REV 105.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 68,697 hrs · 52,647 cycles

FAILSAFE ANGLE ON BELT FRAME DAMAGED AT BS 986.5 BETWEEN S24R - S25R. FAILSAFE ANGLE ON BELT FRAME AT FS 986.5 REPLACED IAW BOEING DWG 6546564 REV AB.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON BELT FRAME TO SKIN ATTACH ANGLE BS 344 S26R - S27R. CORROSION ON BELTFRAME SKIN ATTACH ANGLE STA 344 STR 26R27R BEYOND LIMITS, MADE LIKE REPAIR PART IAW B737 SRM REV 105 CHAPTER 51101 PG 910. INSTALLED IAW CHAPTER 51302.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON STRINGER FITTING 27L AT BS 1016 IN AFT CARGO PIT EQUIPMENT BAY. CORROSION ON STRINGER FITTING 27L AT FS 1016, BEYOND ALLOWABLE LIMITS, NEW FITTING INSTALLED IAW BOEING DWG 6549574 REV D.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACKED INTERCOSTAL FLANGE AT BS 348 S16L & ALSO A CRACKED ANGLE STIFFENER AT SAME LOCATION BS 348L. CRACKED INTERCOSTAL FLANGE AT STA 348 LEFT STRINGER 16 & CRACKED ANGLE STIFFENER AT SAME LOCATION 348 LEFT. REPLACED IAW BOEING 737 SB 737-53A1240 REV 1, ALL FASTENERS INSTALLED IAW B737 SRM 51-30-02 REV 105.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON STRAP ATTACHED TO LOWER FLOORBEAM CAP AT BS 767 LBL 45. CORROSION ON STRAP ATTACHED TO LWR FLOORBEAM CAO AT STA 767 LBL 45, WAS BEYOND LIMITS AND REPLACED PART IAW B737200 SRM 51101 PARAGRAPH 7 REV 105 AS PER ORIGINAL.

Part: BELTFRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON BELT FRAME ATTACH BS 328 S27R. CORROSION ON BELTFRAME ATTACH STA 328 STR 27R REMOVED AND FOUND TO BE BEYOND LIMITS. REPAIRED IAW B737200 SRM 53104 FIGURE 6 PG 1315 REV 105.

Part: SKIN — CRACKED (L2 DOOR) · airframe 68,696 hrs · 52,647 cycles

CRACK IN SKIN, LOWER FORWARD CORNER OF L2 DOOR BS 950 WL 208.1. CRACK IN SKIN LOWER FWD CORNER OF LEFT AFT ENTRY DOOR STA 950 WL 208.1. REPAIRED IAW SERVICE BULLETIN 737531074 REV 3 & BOEING 737200 SRM 53303 FIG 24 REV 105.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON STRINGER 26R BETWEEN BS 1006 AND BS 1016 IN EQUIPMENT BAY OF AFT CARGO PIT. CORROSION ON STRINGER 26R BETWEEN STA 1006 AND 1016, BEYOND ALLOWABLE LIMITS, NEW STRINGER FABRICATED AND INSTALLED IAW B737 SRM REV 105 CHAPTERS 53102 FIG 9 (STRINGER ID) AND 51302 (FASTENER INSTALLATION).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION OF FLOORBEAM BS 348 RBL 14 - RBL 16 TOP SEVERAL LOCATIONS AND AROUND ANCHOR NUTS. CORROSION ON FLOORBEAM STA 348 RBL 14-16 TOP CHORD SEVERAL LOCATIONS & AROUND A/NUTS REMOVED IAW B737-200 SRM 51-10-06 REV 105. NOMINAL THICKNESS WAS .080 REMOVED .030, REMAINING THICKNESS OF .050 BEYOND ALLOWABLE LIMITS IAW BOEING 737-200 SRM 53-10-1 FIGURE 1 REV 105 REPLACED TOP CORD OF FLOORBEAM STA 344 IAW BOEING 737-200 SRM 53-10-2 FIGURE 7 AND WITH B737-200 SRM 53-10-9 FIGURE 5 REV 105 WITH BOEING DRAWING 65-45815 REV L SHEET 5.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

ONE SHEARED RIVET AND CORROSION AT BS 1016 BL 0 AT STIFFENER TO SKIN ATTACH LOWER AREA (ACCESS BELOW FLOOR). ONE SHEARED RIVET AND CORROSION AT STA 1016 BL 0 AT STIFFENER TO SKIN ATTACH LWR AREA, CORROSION FOUND TO BE BEYOND LIMITS, DAMAGE REPAIRED IAW BOEING DWG 65C28106 REV NC.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CORROSION ON BROWNLINE BS 420 - BS 470; LBL 45. CORROSION ON BROWNLINE FS 420 - 470 LBL 45 REMOVED IAW BOEING 737 SRM 511006 REV 105, BEYOND LIMITS IAW B737 SRM 53101 FIG 1 REV 105 NOMINAL THICKNESS .080" REMAINING .055" ALLOWABLE CLEANUP .008", REPLACED CORRODED BROWNLINE AREA IAW B737 SRM 53102 FIG 7 REV 105 AND B737 SRM 53105 FIG 2 REV 105.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON FLOORBEAM. BS 328 RBL 12 - RBL 18 TOP VARIOUS LOCATIONS AND AROUND ANCHOR NUTS. REPLACED FLOORBEAM AT STA 328 RBL WITH REPLACEMENT OF PARTS & REPAIRED IAW B737200 SRM REV 105 53109 FIG 5 SHTS 14.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACK IN LOWER CHORD ORIGINATING FROM AFT HOLE AT RBL 24.82 STA 663. REPAIRED IAW BOEING MESSAGE KFCNAC13000105B AND B737 SRM REV 105 513002. BOEING MESSAGE DATE 2013 JAN 22.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,696 hrs · 52,647 cycles

CORROSION ON FLOORBEAM BS 312 LBL 12 ALSO ON INTERCOSTAL SAME LOCATION AND AROUND ANCHOR NUTS. CORROSION ON FLOORBEAM STA 312 LBL 12 AND ON INTERCOSTAL SAME LOCATION AND AROUND A/NUTS REMOVED IAW B737200 SRM 511006 REV 105, NOMINAL THICKNESS .080" REMOVED .013" REMAINING .067" BEYOND ALLOWABLE LIMITS IAW B737200 SRM 53101 FIG 1 REV 105, REPLACED TOP CHORD OF FLOORBEAM STA 312 RBL 12 LBL 24 IAW B737200 SRM 53102 FIG 7 AND 53109 FIG 5 REV 105, WITH BOEING DWG 6545810 REV K SHEET 5. INTERCOSTAL AND AROUND A/NUTS NOMINAL THICKNESS .080" REMOVED .008" REMAINING .072" WITHIN LIMITS IAW B737200 SRM 53101 FIG 1 REV 105. APPLIED PROTECTIVE TREATMENT IAW B737200 SRM 511002 REV 105.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,696 hrs · 52,647 cycles

CRACKED UPPER FLANGE OF FLOOR INTERCOSTAL AT BS 344 RBL 24. REPLACED CRACKED UPPER FLANGE OF FLOOR INTERCOSTAL AT STA 344 RBL 24 WITH MADE REPAIR PART IAW B737200 SRM REV 105 51201 FIG 7 MATERIAL IDENTIFIED AS 7075T6 .040 IAW SRM REV 105 53102 FIG 7 SHT 7 BAC14902760. INSTALLED FASTENERS IAW SRM 513002 FIG 3 REV 105.

Part: SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 67,182 hrs · 51,429 cycles

ABORTED TAKEOFF DUE TO AFT CARGO LIGHT ILLUMINATED. INSPECTED AFT CARGO DOOR, OPENED AND RE-SECURED DOOR, LIGHT WENT OUT. INSPECTED ALL OTHER DOORS AND PRESSURIZED AIRCRAFT ON GROUND, NO LIGHTS. REAR CARGO DOOR LIGHT DEFERRED PER MEL 52-3 CAT C. MEASURED AFT CARGO COMPARTMENT DOOR SENSOR GAP AT .228, MAX ALLOWABLE IS .220. SHIMMED AFT CARGO COMPARTMENT DOOR SENSOR TO .148 PER B737-200 AMM SEC. 52-71-00 PG 501. OPS CHECK GOOD.

Part: MIXING VALVE — FAILED (RT A/C PACK) · airframe 66,977 hrs · 51,239 cycles

ABORTED TAKEOFF DUE TO RIGHT DUCT OVERHEAT. REPLACED RT PACK AIR MIX VALVE. BACMM 21-61-11-401. OP CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 65,705 hrs · 50,157 cycles

ABORTED TAKEOFF DUE TO MASTER CAUTION, RIGHT DUCT OVERHEAT. CHECKED RIGHT ENGINE DUCTS & LEADING EDGE FOR LEAKAGE. NONE FOUND. COLD CABIN CAUSED RAPID CALL FOR HEAT IN AUTO. TESTED GOOD PER B737-200 AMM 21-61-0-501.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

MINOR CORROSION ON EXTERNAL SKIN UNDER LOWER ATC/MODE S ANTENNA BS 355, BL 0. REPAIRED IAW FAA FORM 8100-9, REF: ID:201101190084-0002D1; FUSELAGE SKIN REPAIR BETWEEN BS 340-360, S-27L TO S-27R (FIRST AND SECOND STAGE APPROVAL).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

FLOOR SUPPORT AT BS 270 BL 0 HAS MINOR CORROSION. CORROSION ON FLOOR SUPPORT AT BS 270 BL 0 WAS FOUND TO BE BEYOND LIMITS IAW B737 SRM 53-10-1. REPAIRED FLOOR SUPPORT IAW B737 SRM 51-40-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACK ON FRAME AFT CARGO PIT, STA 847 AT LWR DOOR STOP, BETWEEN STR 23R & 24R. REPAIRED CRACK ON FRAME AFT CARGO PIT STA 847 AT LOWER DOOR STOP BETWEEN STR 23R & STR 24R. REPAIRED IAW SB737-53-1096, GROUP 3, FIG 3 PG 27 REV 5.

Part: STRAP — CORRODED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CORROSION ON STRAP ON UNDERSIDE OF FRAME STA 794 STR 25R. SPLICED IN NEW STRAP ON UNDERSIDE OF FRAME STA 794 STR 25R IAW BOEING 737 SRM 51-40-3 FIG 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CORRODED SHEAR TIE AT STA 1006 BETWEEN STR 27L AND STR 27R. REPLACED AND INSTALLED NEW SHEAR TIE AT STA 1006 BETWEEN STR 27L AND STR 27R IAW B737 DRW 65-46567, ID:0004, REV C.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACKED STRINGER CLIP IN AFT PIT AT STR 20R STA 867. REPLACED CLIP IN AFT PIT AT STR 20R STA 867 IAW B737 DWG 65-46555 SHEET 9 REV A.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACK ON WING BOX UPPER SKIN STIFFENER AT FS 727, RBL 7. FABRICATED AND INSTALLED WING BOX UPPER SKIN STIFFENER AT FS 727 RBL 7 IAW B737 DWG 65C18354 REV A SHEET 1 AND BOEING SMAL REQUEST.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACKED INTERCOSTAL UNDER DUST SILL STA 500 AT STR 26R. FABRICATED & INSTALLED PART 69-41473-10 INTERCOSTAL UNDER DUST SILL AT STA 500 AT STR 26R IAW B737 DWG 69-41473 SHEET 2 REV A.

Part: RIB — CRACKED (RT WING) · airframe 65,466 hrs · 49,932 cycles

CRACK ON RIB, L/E OF RIGHT WING STA 205. REPAIRED CRACK ON RIB, L/E OF RIGHT WING STA 205 IAW B737 SRM 51-40-3 FIG 1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACKED INTERCOSTAL UNDER DUST SILL STA 500 STR 26L. FABRICATED AND INSTALLED PART 69-41473 INTERCOSTAL AT STA 500 STR 26L IAW B737 DWG 69-41473 SHEET 2 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACK IN INTERCOSTAL UNDER DUST SILL STA 400 STR 26R. REPLACED CRACKED INTERCOSTAL UNDER DUST SILL STA 400 STR 26R IAW DWG 69-41473 REV P.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACK FOUND AT STR 11L ATTACHMENT CLIP AT BS 294 TO 303. REPLACED ATTACHMENT CLIP AT STR 11L AT BS 294 TO BS 303 IAW B737 DRW 65-17684, SHEET 5 REV K & DRW 66-14210 SHEET 1 PART 66-14210-1 ON SHEET 1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACKED L-ANGLE IN LEFT AIR CONDITIONING EQUIPMENT BAY AT STA 639. FABRICATED AND INSTALLED NEW L-ANGLE IN LEFT AIR CONDITIONING EQUIPMENT BAY AT STA 639, LBL 6.5 IAW B737 DWG 65-45866 SHEET 19, DWG 65-51555 FOR INSTALLATION.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACK DETECTED BY NDT REPORT NDT 11-0014 AT FS 303.9 STR 16L ON THE WEB AT THE STRINGER CUT OUT. REPAIRED WEB AT FS 303.9 STR 16L IAW SB737-53A1197 FIG 3, FIG 4 DATED 2006 AUG 25.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CORRODED CLIP AT STA 847 RBL 24 UNDER AFT CARGO PIT DOOR FRAME. REPLACED CLIP AT STA 847 RBL 24 UNDER AFT CARGO PIT DOOR FRAME IAW B737 DWG 65-47960 REV Y.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

DAMAGED STRINGER CLIP AT STA 380L STR 19L. DAMAGED STRINGER CLIP AT STA 380L STR 19L REPLACED IAW BOEING 737 DWG 65-46525 REV J.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACK IN FUSELAGE SKIN AT STA 727B - 733, STR 181L. REPAIRED CRACK IN FUSELAGE AT STA 727B-733 IAW B737-200 SRM 53-30-3 FIG 48, DETAIL XI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

CRACK INDICATION AT RADIO ALTIMETER BETWEEN BS 400 - 420 AS PER NDT REPORT NDT11-0027. REPAIRED CRACK AT RADIO ALTIMETER BETWEEN BS 400-420 IAW SB 53-1230 DATED 12 JUNE 2002 PER TABLE C, FIG 9 & 10.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

REPLACE CRACKED STRINGER CLIPS PER ATTACHED MTC-120 IAW BOEING SB 737-53-1268. SQUAWK GENERATED BY AD 2009-04-15 PARA F. REPLACED CRACKED STRINGER CLIPS AS PER ATTACHED MTC-120 FORMS, STN 597 STR 7L, STN 616 STR 5L, STN 639 STR 4L, STN 706 STR 10L, STN 727B STR 4L, AND STN 727B STR 8R. IAW B737 SB 53-1268 DATED 25 AUG 2006, FIGURES 16 & 32; NO OVERSIZED FASTENERS USED TO INSTALL NEW STRINGER CLIPS.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 65,466 hrs · 49,932 cycles

DAMAGED STRINGER CLIP AT STA 380L STR 21L. REPLACED STRINGER CLIP AT STA 380L STR 21L IAW B737 DWG 65-46525, REV J.

Part: BUNGEE — BROKEN (NLG) · airframe 64,353 hrs · 48,921 cycles

NOSE GEAR WOULD NOT EXTEND, LOSS OF HYDRAULIC QUANTITY, GEAR MANUALLY EXTENDED. FOUND BROKEN BUNGEE SPRING, BROKEN DOWN LINE AND DAMAGE TO BULKHEAD. REPLACED BUNGEE SPRING REF B737-200 MM 32-33-51, INSTALLED SERVICEABLE NOSE LANDING GEAR DOWN LINE REF B737-200 MM 20-10-51, AND REPLACED DAMAGE PANEL REF SRM 737-200 51-30-2. OP CHECKED GEAR IAW B737-200MM SEC 52-33-0, OPERATIONAL AND LEAK CHECKED GOOD.

Part: FUSE — BROKEN (HYDRAULIC SYS) · airframe 64,283 hrs · 48,861 cycles

A SYSTEM HYDRAULIC QUANTITY LOSS. FOUND STUB LINE AT MAIN LANDING GEAR HYDRAULIC FUSE BROKEN. FABRICATED AND INSTALLED REPLACEMENT LINE AND PERFORMED LEAK CHECK WITH NO FURTHER DEFECTS NOTED. REF B737-200 MM 20-10-51 PAR 801.

Part: STRINGER CLIP — CRACKED (BS 947 S29R) · airframe 61,849 hrs · 46,721 cycles

BS 947 S26R CLIP CRACKED. FABRICATED AND REPLACED STRINGER CLIP AT STA 947 STR 26R WITH FABRICATED REPAIR PART IAW SRM 51-10-01, 51-20-01, 51-30-02, 51-10-02, 51-21-00.

Part: SUPPORT ANGLE — CRACKED (BS 296) · airframe 61,849 hrs · 46,721 cycles

L1 DOOR OPENING SUPPORT ANGLE CRACKED AT STA 296, STRINGER 12L. REPLACED CRACKED SUPPORT ANGLE AT L1 DOOR OPENING AT STA 296, STRINGER 12L IAW SRM 51-10-01. FASTENERS INSTALLED IAW 51-30-02. INSTALLED ANGLE IAW KEL-NAC-09-0002-08, B AND DRAWING 65C38823.

Part: FRAME — CRACKED (BS 492) · airframe 61,849 hrs · 46,721 cycles

CRACKED FRAME AT BS 492 STR 22R RIGHT BELOW 40. REPLACED CRACKED FRAME AT BS 492 WITH P/N 65-20723-29 IAW DRAWING NR 65-20723, REV D AND 737-20 SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (BS 294)

CRACK ON FWD ATTACH INTERCOSTAL STA 294 STR 7L. REPLACED INTERCOSTAL IAW B-737 SRM 51-10-01, SEC 7. FASTENERS INSTALLED IAW 51-30-02, INSTALLED INTERCOSTAL IAW KEL-NAC-09-0002-08B AND DRAWING 65C38823.

Part: SUPPORT ANGLE — CRACKED (BS 300) · airframe 61,849 hrs · 46,721 cycles

L1 DOOR OPENING SUPPORT ANGLE CRACKED AT STA 300 STRINGER 10L. REPLACED CRACKED SUPPORT ANGLE AT STA 300 STRINGER 10L IAW SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02. INSTALLED ANGLE IAW KEL-NAC-09-0002-088, AND DRAWING 65C38823, STEP 4.

Part: STRINGER CLIP — CRACKED (BS 360 S10L) · airframe 61,849 hrs · 46,721 cycles

CRACK ON AFT ATTACH CLIP OF INTERCOSTAL STA 360 STR 10L. REPLACED CRACKED ATTACH CLIP IAW B737 SRM 51-10-01. FASTENERS INSTALLED IAW 51-30-02. INSTALLED INTERCOSTAL IAW KEL-NAC-09-0002-08B, AND DRAWING 65C38823, STEP 3.

Part: SKIN — CORRODED (BS 480) · corrosion level 2 · airframe 61,849 hrs · 46,721 cycles

CORROSION ON SKIN FWD CARGO DOOR LOWER CUTOUT STA 480, STRINGER 23R. REPAIRED SKIN ON FWD CARGO LOWER CUTOUT STA 480, STRINGER 23R IAW SRM 53-30-03 DETAIL IV, CORROSION REMOVAL BEYOND LIMITS, MATERIAL REMOVED .059, MAXIMUM ALLOWABLE MATERIAL TO BE REMOVED .011.

Part: STRINGER SPLICE — CRACKED (BS 907) · airframe 61,849 hrs · 46,721 cycles

CRACK AT BS907 STR 4L STRINGER SPLICE. REPLACED STRINGER SPLICE AT BS907 STR 4L IAW SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02.

Part: STRINGER SPLICE — CRACKED (BS 540 S10R) · airframe 61,849 hrs · 46,721 cycles

STRINGER CRACKED AT STA 540, STR. 10R. REPLACED CRACKED STRINGER SPLICE AT STA, 540, STR. 10R IAW B737 SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02.

Part: STRINGER SPLICE — CRACKED (BS 907 S4R) · airframe 61,849 hrs · 46,721 cycles

CRACK AT STA 907, STR 4R STRINGER SPLICE. REMOVED AND REPLACED CRACKED STRINGER SPLICE AT STA 907 STR 4R IAW SRM 51-10-01 SECTION 7, FASTENERS INSTALLED IAW 51-30-2.

Part: SKIN — DETACHED (BS 1016) · airframe 61,849 hrs · 46,721 cycles

LARGE GAP ON UNDERSIDE OF REPAIR AT STA 1016 BETWEEN STR 20R AND 21R. REPLACED WITH NEW REPAIR AT STA 20R-21R IAW B737 SRM PG.S 253-309 FIG. 48 DETAIL XXX.

Part: DOOR FRAME — CORRODED (E/E BAY) · corrosion level 2 · airframe 61,849 hrs · 46,721 cycles

E AND E COMPARTMENT DOOR FRAME, RT SIDE, OTBD OF DOOR PIN STRUCTURE VERTICAL ANGLE CORRODED. REPLACED CORRODED ANGLE ON E AND E COMPARTMENT DOOR FRAME RT SIDE OTBD OF DOOR PIN STRUCTURE IAW SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02.

Part: SKIN — CRACKED (FUSLEAGE) · airframe 60,279 hrs · 45,213 cycles

FUSELAGE SKIN CRACKED AT STRINGER 21R, BS 931-BS 934.0625. CRACK IS 3.0625" LONG. REPAIRED PER BOEING REPAIR SKETCH AND SERVICE REQUEST MESSAGE 1-79197357-1 THRU -21, FAA FORM 8100-9, DATED 21 MARCH 2008. 8100-9 STATES ALTERNATE REPAIR HAS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (D) OF AD 2004-18-06.

Part: ACTUATOR — FRACTURED (SPOILERS) · airframe 59,428 hrs · 44,394 cycles

"A" SYSTEM HYDRAULIC FAILURE ON GROUND. REMOVED AND REPLACED NR 8 SPOILER ACTUATOR DUE TO HOUSING FAILURE. LEAK CHECK, FUNCTIONAL CHECK AND SPOILER TO FLAP CLEARANCE CHECKED GOOD. REF: B737MM 27-62-101.

Part: SKIN — SCRATCHED (BS 1088) · airframe 58,701 hrs · 43,689 cycles

AFT FUSELAGE HAS A SCRATCH AT BS 1088, BETWEEN SR 20 AND SR 23. CUT OUT DAMAGED AREA AT AFT FUSELAGE BS 1088 BETWEEN SR 20 AND SR 23 AND FABRICATED REPAIR DOUBLER IAW JOSSAIR DRAWING NR 73R5331545 REV I/R DATED 17 FEB 2007.

Part: SKIN — CORRODED (BS 767-787) · corrosion level 2 · airframe 58,701 hrs · 43,689 cycles

AFT CARGO COMPARTMENT BILGE AREA HAS SURFACE CORROSION AT STA 787 BETWEEN STR 27L AND STR 27R. REMOVED CORROSION, PERFORM ULTRASONIC THICKNESS TEST AND FOUND OUT OF LIMITS PER B737 SRM 53-30-1. FABRICATED REPAIR DOUBLER AND INSTALLED AT FUSELAGE SKIN BS767 - BS787, L-26L - L-26R PER JOSSAIR DRAWING NR 73R5331458 REV I/R DATED 12 JAN 2007.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 58,701 hrs · 43,689 cycles

FOUND LT HORIZONTAL STAB LOWER SURFACE DAMAGED, "HAS HOLE". REPAIRED DAMAGED AREA PER JOSSAIR DRAWING NR 73R5511546 REV A DATED 21 FEB 2007. "CUTOUT REPAIR AT STABILIZER BOTTOM SKIN-STAB STA 111.0-STA 120.0".

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 57,909 hrs · 43,105 cycles

SUSPECT BIRD INGESTION ON TAKEOFF FELT SMALL SHUDDER AND HEARD SOUND FOLLOWED BY FOUL ODOR. ENGINE PARAMETERS NORMAL. PERFORMED MTC INSPECTION PER MM 05-51-201-201. PS 3 FILTER NR 1 ENG CLEAN. RAN ENGINE TO T/O PWR ALL PARAMETERS NORMAL. NO ODORS IN A/C. A/C OK FOR SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 53,945 hrs · 40,083 cycles

SKIN GOUGE CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND GOUGED NEAR THE FWD EDGE OF THE C1 DOOR CUTOUT BETWEEN FS 430 AND 440 AT STRINGER 22R. THE DAMAGE WAS REMOVED WITH A 10.5 X 1.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 385464-14, REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,455 hrs · 39,669 cycles

AFT ENTRY DOOR CUTOUT, UPPER HINGE CUTOUT CRACK REPAIR THE UPPER HINGE CUTOUT OF THE L2 DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK THROUGH THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385034-14, REV A.

Part: DUCT — FOD (RT PACK) · airframe 52,905 hrs · 39,203 cycles

A/C DIVERTED TO ATL EN ROUTE BHM TO CVG WITH RIGHT PACK TRIP OFF AND DUCT OVERHEAT SHORTLY AFTER T/O FROM BHM. PROCEDURES RAN AND PACK RESET SUCCESSFULLY. SHORTLY THEREAFTER HAD FUMES IN ENTIRE AIRPLANE. RAN SMOKE/FUMES PROCEDURE WITH NO AVAIL. OPERATED RT PACK ON GROUND IN ATL WITH NO OVERHEAT OR ABNORMALITIES. REMOVED DEBRIS FROM DUCT.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 52,243 hrs · 38,904 cycles

DURING CLIMB CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE ABOVE 10000 FT CABIN VSI +500/MIN IN AUTO MODE WITH NO WARNING LIGHTS OR FAILURE OF AUTO MODE SHOWING. CABIN ALTITUDE CONTROLLED WITH MANUAL CONTROL. REPLACED CABIN PRESS CONTROLLER AND CONTROL PANEL PER M/M AND PERFORMED OPERATIONAL TEST AND CABIN LEAK DOWN CHECK NTF.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,457 hrs · 38,569 cycles

FORWARD OUTBOARD F/A FLASHLIGHT BATTERY LOW. REPLACED BATTERY, CHECKS OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,657 hrs · 37,817 cycles

DENT DAMAGE WAS FOUND DURING HMV ON THE FUSELAGE SKIN AT FS 440 AND STR 22R TO 24R. A PREVIOUS DOUBLER REPAIR WAS LOCATED IN THE AREA, THEREFORE THE PREVIOUS REPAIR WAS REMOVED AND A NEW DOUBLER/TRIPLER REPAIR WAS INSTALLED. ER/A 257875-14, REV E.

Part: TRACK — CORRODED (TE FLAP) · airframe 49,657 hrs · 37,817 cycles

THE REAR ENGINE MOUNT ATTACH HOLES ON THE #2 AND #3 TE O/B FLAP TRACKS WERE FOUND CORRODED. THE BORES WERE OVERSIZED TO .939" AND NEW BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 49,657 hrs · 37,817 cycles

CORROSION WAS FOUND IN THE VERTICAL STABILIZER ATTACH LUG BORES. ER/A 398140-14AD.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 49,657 hrs · 37,817 cycles

FWD CARGO DOOR LWR FWD AND AFT FRAMES WERE FOUND CRACKED. REPAIRED PER ER/A 410587-14AD.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 49,287 hrs · 37,658 cycles

EMERGENCY LIGHT AT ROW 19DEF INOP. REPLACED LIGHT SOCKET IN SEAT ROW.

Part: INDICATOR — FAILED (COCKPIT) · airframe 48,633 hrs · 37,377 cycles

ABORTED T/O DUE TO NR 2 EGT FAILED TO ZERO AT T/O POWER, APPROX 50 KTS. RETURNED TO GATE. REPLACED NR 2 ENGINE EGT INDICATOR. RAN ENGINE TO T/O POWER. ALL INDICATIONS CHECK NORMAL. EGT OPN NOW OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,435 hrs · 37,290 cycles

ON SERVICE CK, FOUND CABIN OVERWING EXIT SIGN INOP FOR CENTER AISLE. REPLACED BATTERY PACK PER M/M, CKS OK.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,329 hrs · 37,244 cycles

THE LONGITUDINAL FLOORBEAM OVER THE CENTER WING BOX AT BL 0 WAS FOUND WITH A CRACK IN THE FLOORBEAM WEB AND UPPER CHORD AT FS 660 AND 2 CRACKS IN THE FLOORBEAM WEB AT FS 705. THE CRACKED BEAM WAS REPAIRED PER BAC S/B 737-57-1210 AND ER/A 380765-14.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,329 hrs · 37,244 cycles

THE LBL 24 LONGITUDINAL FLOORBEAM OVER THE CENTER WING WAS FOUND WITH A CRACK IN THE BEAM WEB DOUBLER AT FS 678. THE CRACKED WEB DOUBLER WAS REMOVED. A NEW WEB DOUBLER WAS INSTALLED AND THE BEAM MODIFIED PER BAC S/B 737-57-1139. THE REPAIR WAS ACCOMPLISHED PER ER/A 380725-14, REV A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,329 hrs · 37,244 cycles

THE LONGITUDINAL FLOORBEAM OVER THE CENTER WING AT RBL 24 WAS FOUND WITH A CRACK IN THE BEAM WEB DOUBLER AT FS 678 AND IN THE FLOOR BEAM UPPER CHORD AT FS 674. THE CRACKED WEB DOUBLER AND UPPER CHORD WERE REMOVED. A NEW WEB DOUBLER AND CHORD WERE INSTALLED ALONG WITH THE BEAM MODIFICATION PER BAC S/B 737-57-1139. THE REPAIR WAS ACCOMPLISHED PER ER/A 380722-14, REV A.

Part: TORQUE TUBE — STUCK (ELEVATOR) · airframe 48,013 hrs · 37,110 cycles

ELVEATOR JAMMED AND STUCK IN FLIGHT CONTINUED STICKING AND RELEASING THROUGH REST OF FLIGHT DIVERTED TO ATL TRIED ISOLATED A AND B DID NOT HELP. REPLACED ELEVATOR INPUT TORQUE TUBE

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,561 hrs · 36,922 cycles

EMERGENCY ESCAPE PATH LIGHTS SEAT ROW 1 TO 4 AND CLOSET LIGHTS INOP. REPLACED BATTERY AND POWER SUPPLY.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,146 hrs · 36,749 cycles

FUSELAGE / SKIN ASSY / FS 960-1000 / STRG. 21L-25L : GROUND DAMAGE REPAIR. THE FUSELAGE SKIN AND UNDERLYING FRAMS AND STRINGERS WERE BADLY DAMAGED BY GROUND EQUIPMENT IMPACT BETWEEN FS 960 & 1000 AND BETWEEN STRINGERS 21L & 25L. THE DAMAGED AREAS OF STRINGERS 22L-24L WERE REMOVED AND NEW SECTIONS SPLICED IN. THE FS 967 & 987 LOWER FRAME SECTIONS WERE REPLACED. A NEW SECTION OF SKIN WAS INSTALLED. THE REPAIRS WERE ACCOMPLISHED PER ER/A 379489-14, REV A.

Part: TERMINAL — LOOSE (CABIN) · airframe 46,910 hrs · 36,649 cycles

LEFT AISLE EMERGENCY LIGHTS (AFT 3 LAMPS) INOP. FOUND GROUND TERMINAL LOOSE. TIGHTENED SAME AND OPERATION NORMAL.

Part: CONTROLLER — MALFUNCTIONED (MLG WW) · airframe 44,875 hrs · 35,746 cycles

ON APPROACH WITH B A/P ENGAGED UPON DEPLOYMENT OF SPEEDBRAKES HAD UNCOMMANDED ROLL. REPLACED SPOILER MIXER PER M/M AND TESTED YAW DAMP SYSTEM AS PRECAUTION.

Part: SKIN — CRACKED (PAX DOORWAY)

THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT WAS FOUND WITH A 3.25 INCH LONG CRACK IN THE SKIN, BONDED DOUBLER, AND UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT AND AN ALUMINUM REPAIR DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 365222-14, REV A. THE DAMAGED AREA IS WITHIN THE SSI F-17 REGION.

Part: WIRE — SHORTED (CABIN)

FOUND LAST 3 SEAT ROWS EMERG EXIT LIGHTS INOP. FOUND ON NR 2 L/O. REPAIRED WIRING.

Part: SKIN — CRACKED (R1 DOORWAY)

THE SKIN OF THE R1 DOOR LOWER HINGE CUTOUT WAS FOUND WITH A CRACK APPROXIMATELY .375 LONG. REPAIRED PER DELTA ER/A 330837-14, REV A.

Part: INTERCOSTAL — CRACKED (BS 334)

R1 DOOR FRAME INTERCOSTAL AT S8A FOUND CRACKED. REPAIRED PER ERA 330806-14AD.

Part: SKIN — DENTED (BS 915)

A DENT FOUND IN THE FUSELAGE SKIN AT APPROX FS 915 JUST BELOW S22R. THE DENT WAS REMOVED WITH A 2.5 BY 1.25 CUTOUT. REPAIRED PER ERA 330830-14.

Part: PWR SUPPLY — INOPERATIVE (CABIN)

EMERGENCY AISLE LIGHT 12 ABC INOP. REPLACED PWR SUPPLY ASSY 036, OPS OK.

Part: WIRE — LOOSE (RT MLG SENSOR)

DEPARTING, LNDG GEAR HANDLE WOULD NOT MOVE. FOLLOWED POM PROCEDURES, WARNING HORN REMAINS ON WHEN FLAPS UP INDICATES AIR/GRD SENSORS IN GROUND MODE. RETERMINATED GRD WIRE FOR PROX SWITCH S106 GEAR AIR SENSE GEAR HANDLE, OPERATION NORMAL. L.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON L/O, FOUND MID CABIN OVERHEAT EMERGENCY LIGHT AND LIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CKS NORMAL.

Part: BULKHEAD — CRACKED (BS 178)

TWO CRACKS WERE DISCOVERED ON FWD FACE OF THE F.S.178 BLKHDWEB. TWO INDEPENDENT CUTOUTS WERE REQUIRED TO REMOVE THE CRACKS. FIRST CUTOUT, LOCATED INBD OF THE RBL 5.7 VERTICAL STRAP AT WL 200, MEASURES 4.0 INCH VERTICALLY BY 1.0 INCH INBD/OTBD. THE SECOND CUTOUT IS LOCATED AT THE LBL 5.7 VERTICAL STRAP AT WL 200 AND MEASURES 4.0 INCHES VERTICALLY BY 1.0 INCH INBD/OTBD. REPAIRED PER ERA 304394-14 REV A.

Part: GEAR MODULE — MALFUNCTIONED (LANDING GEAR)

UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF FROM CVG. ALSO, T/R REV ILLUM MSG ON IN FLT. REPLACED LANDING GEAR MODULE AND CKD PER M/M CHAP 32 AND RESERVICED RT MAIN STRUT, JACKED A/C AND CKS OK.

Part: MODULE — NOT SEATED (LANDING GEAR)

AIRCRAFT RETURNED CVG AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT. RESEATED LANDING GEAR MODULE AND SWUNG GEAR, ALL CHECKS NORMAL.

Part: SENSOR — FAILED (RT MLG)

SHIP 321 WAS OFF AND RETURNED WITH RT GEAR UNSAFE LIGHT. FOUND RT MAIN GEAR SENSOR S73 BAD. REPLACED SAME AND OPS NORMAL.