N615AS

Part: STIFFENER — CRACKED (ZONE 100) · airframe 75,247 hrs · 39,997 cycles

VAPOR BARRIER STIFFENER P/N 111A1301-5 CRACKED EDGE TO EDGE NEAR INBD ATTACH HARDWARE. GROUNDED - YES. REMOVED AND INSTALLED NEW VAPOR BARRIER STIFFENER PN: 111A1301U5. BATCH# 0004423293 AT STA 650-STA663 LH MLG LOWER VAPOR BARRIER AT LBL 6.15 IAW B737-700 SRM 51-40-02-06-0 REV 86-10JUL2025.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 75,040 hrs · 39,844 cycles

EMERGENCY LIGHTS AT LT OVERWING EXIT INSIDE AND OUTSIDE AND ROW 7 ABC DID NOT PASS 15 MINS CAPACITY CHECKS. GROUNDED - YES. REPLACED M1668 EMERG EXIT LIGHT BATT PACK POWER SUPPLY FOR LH OVERWING EXIT INSIDE AND OUTSIDE LIGHTS AND ROW 7 ABC LIGHTS, OPS NML REF MM 33-51-06-960-805 AND REF WDM 33-51-13.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 74,344 hrs · 39,340 cycles

MULTIPLE EMERGENCY LIGHTS OUT. GROUNDED - YES. EMERGENCY LIGHT BULB REMOVED AND REPLACED IAW BOEING 737-700 AMM 33-51-01-960-801 EMERGENCY LIGHT OPERATIONAL TEST SUCCESSFUL IAW BOEING 737-700 AMM TASK 33-51-00-710-801WO: 2042354REFERENCE_TASK_CARD: 78233000.

Part: COVER — DETACHED (ZONE 200) · airframe 73,392 hrs · 38,659 cycles

EXIT SIGN COVER IN L1 DOOR FELL OFF. GROUNDED - YES. (RESOLVED ON W/O: 2027021 TASKCARD: N/R-00003 ) REMOVED THE TAPE AND REPLACED THE L1 DOOR EXIST SIGN LIGHT ASSEMBLY, REF AMM 33-51-01-960-802 . THIS CLEAR INT DEFERAL C/N 22027615. SEAMC NOTIFIED.

Part: LENS — MISSING (ZONE 200) · airframe 72,997 hrs · 38,397 cycles

L2 DOOR EMERG EXIT SIGN MISSING COVER. GROUNDED - YES. REPLACED L-2 DOOR EMERG EXIT SIGN LENSE COVER. OP'S CK IS GOOD REF AMM 33-51-01.

Part: LIGHT — DETACHED (ZONE 200) · airframe 72,790 hrs · 38,276 cycles

FA'S ADVISED EXIT ROW LEFT SIDE LOWER SIDE SMALL LOWER EXIT LIGHT COVER WILL NOT STAY ATTACHED 17A. GROUNDED - YES. RE-SECURED LH LOWER EMERGENCY EXIT LIGHT COVER PER AMM 33-51-00.

Part: DOUBLER — DAMAGED (DOOR LATCH) · airframe 72,654 hrs · 38,186 cycles

DAMAGE FOUND ON HIGH PRESSURE DOOR LATCH DOUBLER AND SURROUNDING AREA. (REF LP 60953288) GROUNDED - YES. (RESOLVED ON W/O: 2011735 TASKCARD: N/R-00002 ) VERIFIED MATERIAL FOR FILLER AND STRAP AS 0.125" 7075-T6 BATCH # 2654778. TRIMMED OUT DAMAGED SECTION PER SRM 57-10-13-2R-3.15371. PERFORMED HFEC INSPECTION ON CUTOUT EDGE REF 737 NDT PART 6 51-00-00 PROCEDURE 23. PERFORMED HFEC INSPECTION ON ALL INITIAL FASTENER HOLES IN THE REPAIR AREA REF 737 NDT PART 6 51-00-00 PROCEDURE 16. NO INDICATION NOTED.57213. ACC VISUAL INSP OF NUTPLATE ATTACHMENT FASTENER HOLES IAW E.A. 700-57EA-27350. FABED/DRILLED UP REPAIR STRAP AND FILLER AND APPLIED ALODINE AND PRIMER IAW SRM 57-10-13-2R-3.15371.26947. INSTALLED REPAIR PER SRM 57-10-13-2R-3. CLEARED MCT DEFERAL.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 71,780 hrs · 37,600 cycles

EMERGENCY EXIT LIGHT LENS IS DAMAGED AT SEAT ROW 16BC. GROUNDED - YES. REPLACED LENS COVER FOR EXIT FLOOR AT 16BC.

Part: SUPPORT — DAMAGED (ELEVATOR TAB) · airframe 71,301 hrs · 37,262 cycles

OUT OF LIMITS DAMAGE TO ELEVATOR TRIM TAB SUPPORT CHORD, CLEVIS AND CLIP. GROUNDED - YES. FABRICATED NEW CLIP. REMIVED AND REPLACED SUPPORT CHORD AND CLEVIS PER ASA EA 700-55EA-26415, BOEING DWGS 185A1700 AND 185A1212.

Part: STIFFENER — DENTED (HORIZONTAL STAB) · airframe 71,301 hrs · 37,262 cycles

LH HORIZ STAB, STIFFENER ON FWD SPAR AT STAB STA 166.30 GOUGED AND DENTED. GROUNDED - YES. REMOVE SPAR WEB, FABRICATE NEW STIFFENER AND REPLACE. REINSTALL WEB. REF ASA EA 700-55EA-26445 AND BOEING DWG 182A2401.

Part: SKIN — NONE (BS 166.3) · airframe 71,301 hrs · 37,262 cycles

ENGINEERING REQUESTED HOLE FOR ACCESS OF DAMAGE AT STA 166.30. GROUNDED - YES. ACCOMPLISHED REPAIR PER B737-700 SRM 55-10-01-2R-11 AND ASA EA CMPT-55EA-26456.

Part: STIFFENER — DAMAGED (LT ELEVATOR) · airframe 71,301 hrs · 37,262 cycles

FOUND SEVERAL DAMAGED FASTENERS AT TRAILING EDGE RIB FITTING, LH ELEVATOR STA 121.59. FOUND DAMAGED SPAR STIFFENER DURING REPLACEMENT OF FASTENERS GROUNDED - YES. REMOVED AND REPLACED FASTENERS. FABRICATED NEW 182A1505-83 STIFFENER PER ASA EA 700-55EA-26470 AND BOEING DWG 185A1600.

Part: RIB — CORRODED (ELEVATOR) · airframe 71,301 hrs · 37,262 cycles

FRETTING CORROSION FOUND ON RIB AND CLEVIS FITTING AT ELEVATOR STA 176.64 CAUSED BY CRACKED BEAM. GROUNDED - YES. ACCOMPLISHED ASA EA 700-55EA-26434.

Part: BEAM — CRACKED (HORISONTAL STAB) · airframe 71,301 hrs · 37,262 cycles

MULTIPLE CRACKS FOUND ON UPPER CHORDS OF AFT BEAM ON LH HORIZONTAL STABILIZER. GROUNDED - YES. REMOVED AND REPLACED CHORDS PER ASA EA EA700-55EA-26474 AND BOEING DWG 185A1600 ID 9-11 AND 185A1700 ID 4-6

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 70,274 hrs · 36,533 cycles

STA 663 LOWER VAPOR BARRIER LOWER ATTACH ANGLE CRACKED JUST O/B OF R/H KEEL BEAM. GROUNDED - YES. REPAIRED IAW B737-700 SRM 57-10-10-2R-5.

Part: FLOOR SUPPORT — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

AFT CABIN FLOOR SUPPORT STA 947 TO STA 967 LBL 16" SMALL AREA OF CORROSION ON TOP SIDE, MARKED. GROUNDED - YES. REMOVED CORROSION FROM AFT CABIN FLOOR SUPPORT BETWEEN STA 947 AND STA 967 AND FLOOR SUPPORT WAS FOUND TO BE WITHIN LIMITS IAW B737-700 SRM 53-70-51-1A-1.W= 1.5" O= .080" R= .073" L= 3.0" D= .007".

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

L-2 DOOR FLOOR CREASE BEAM AREA OF LIGHT CORROSION, MARKED. GROUNDED - YES. REMOVED DAMAGE L-2 DOOR FLOOR CREASE BEAM FOUND IN LIMITS IAW B737-700 SRM 53-70-15-1A-1.W= .050 O= .080 R= .077 L= .050 D= .003.

Part: CARGO TRACK — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

AFT CARGO PIT CARGO TRACK AT RBL 18 FROM STA 787 TO STA 847 CORRODED. GROUNDED - YES. REMOVED AND REPLACED NEW AFT CARGO PIT CARGO TRACK AT RBL 18 FROM STA 787 TO STA 847 IAW B737-700 SRM 51-40-02-0G-0.W= 1" O= .070" R= .052" L= 1" D= .018".

Part: WEB — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

AFT CARGO PIT CARGO DOOR WEB SILL CORRODED. GROUNDED - YES. REMOVED DAMAGE TO AFT CARGO PIT CARGO DOOR WEB SILL FOUND TO BE IN LIMITS IAW B737-700 SRM 53-60-15-1A-1.W= 1" O= .045 R= .043 L= 2" D= .002.

Part: TRANSITION PANEL — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

AFT CARGO PIT RH TRANSITION CORRODED FROM STA 727B TO STA 767. GROUNDED - YES. REMOVED DAMAGE ON AFT CARGO PIT R/H TRANSITION FROM STA 727B TO STA 767 FOUND TO BE IN LIMITS IAW B737-700 SRM 53-00-53-1A-2. W= 1" O= .040 R= .038 L= 1" D= .002.

Part: TRANSITION PANEL — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

FWD CARGO PIT LH TRANSITION CORRODED FROM STA 500A TO STA 500D. GROUNDED - YES. REMOVED AND REPLACE FWD CARGO PIT LH TRANSITION FROM STA 500A TO STA 500D IAW B737-700 SRM 51-40-02-0G-0.W=1" O= .040 R= 0 =1" D= .040.

Part: WEB — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

FWD CARGO PIT CARGO DOOR WEB SILL CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM DOOR WEB SILL FOUND IN LIMITS IAW B737-700 SRM 53-3.0-15-1A-1.W= 1INCH O= .045 R= .042 L= 1" D= .003".

Part: SHIELD — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

AFT CARGO PIT FWD HEAT SHIELD CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE IN LIMITS IAW B737-700 SRM 53-60-15-1A-1.W= 1 INCH O= .050 R= .048 L= 1 INCH D= .002.

Part: TRANSITION PANEL — CORRODED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

AFT CARGO PIT LH TRANSITION CORRODED FROM STA 727C TO STA 847. GROUNDED - YES. REMOVED AND REPLACED AFT CARG L/H TRANSITION FROM STA 727C TO STA 847 IAW B737-700 SRM 51-40-02-0G-0.W= 1 INCH O= .040 R= 0 L= 1 INCH D= .040.

Part: RIB — CRACKED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

R/H HORIZONTAL SPAR CRACKED AT MACHINED STIFFNER AT STAB STA 92.7. GROUNDED - YES. REPAIRED RIB @ STA 92.7 IAW B737-700 SRM 55-10-09-2R-4.

Part: RIB — CRACKED (UNKNOWN) · airframe 70,274 hrs · 36,533 cycles

R/H HORIZONTAL SPAR CRACKED AT MACHINED STIFFNER AT STAB STA 111.10. GROUNDED - YES. REPAIRED RIB @ STA: 111.10 IAW B737-700 SRM 55-10-09-2R-4.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,976 hrs · 36,291 cycles

FWD BULKHEAD BY L1 DOOR EXIT LIGHT COVER FELL OFF. GROUNDED - YES. TIGHTENED LIGHT COVER ON FWD BULKHEAD L1 DOOR REF B737-700 AMM 33-51-01.

Part: HOUSING — DETACHED (L1 DOOR) · airframe 69,701 hrs · 36,076 cycles

L1 DOOR EXIT INDICATOR CAME OFF. GROUNDED - YES. REPLACED L1 DOOR EXIT INDICATOR ASSY REF B737-700 AMM 33-51-01.

Part: BRACKET — LOOSE (L2 DOOR SLIDE) · airframe 69,196 hrs · 35,657 cycles

ON L2 DOOR, SLIDE PACK COVER BRACKET LOOSE/PULLING OUT OF DOOR. GROUNDED - YES. L2 DOOR SLIDE PACK BRACKET IS SECURE NO DEFECT NOTED. FOUND L2 DOOR AFT SLIDE GIRT BAR FLOOR FITTING LOOSE. REMOVED AND REINSTALLED PLOOR FITTING WITH NEW HARDWARE REF B737-700 AMM 25-66-02. OPS GOOD.

Part: TRANSFORMER — BURNED (E/E RACK E4) · airframe 68,184 hrs · 34,891 cycles

"ELEC" LIGHT ON OVERHEAD PANEL ILLUMINATED SHORTLY AFTER LANDING. AFT GALLEY FLIGHT ATTENDANT REPORTED UNUSUAL ODOR COMING FROM VICINITY AS "PLASTICY". LEVEL ONE AIR QUALITY EVENT. GROUNDED - YES. A/C HAS HISTORY OF SAME FAULT REF LOG 60493658. PERFORMED ELEC LIGHT BITE REF B737-700 FIM 24-31 TASK 801. FAULT "BAT CHGR #1" LOGGED. REMOVED AND REPLACED RECIRULATION AIR FILTER REF B737-700 AMM 21-25-01. REMOVED AND REPLACED WATER SEPARATOR COALESCER BAGS ON LEFT AND RIGHT WATER SEPARATORS REF AMM 21-51-05-400-801. EVIDENCE OF TR UNIS 3 AND 2 BURNING FOUND AREA DIRECTLY ABOVE E4-2 RACK COMPONENTS CHARRED (BELOW E4-1 COMPONENTS). REPLACED THE #2 AND #3 TR UNITS PER AMM 24-32-11/401. OPS CHECKS REQ'D REPLACED THE SELCAL DECORDER REF AMM 23-28-11/401. REPLACED THE CABIN TEMP CONTROLLER PER AMM 23-51-01/401. REPLACED THE RH FRONT AND LH SIDE WHCU'S REF AMM 30-41-11/401.

Part: BATTERY — ODOR (E/E BAY) · airframe 68,173 hrs · 34,884 cycles

AT FL360 , JUST BEFORE DESCENT , F/A ADVISES NOTICEABLE ODOR COMING FROM REAR OF THE CABIN. NO SMOKE OR OTHERWISE VISIBLE CONTAMINANT OBSERVED. AFTER LANDING, ELEC AMBER LIGHT ILLUMINATED. LEVEL ONE AIR QUALITY EVENT. GROUNDED - YES. VERIFIED NO VISUAL SMOKE OR FUMES - ODOR NOTED WAS ELECTRICAL IN SMELL . FLT CREW REPORTED APU NOT RUNNING. ELEC BITE SHOWS PRI BATT CHARGER FAULT. INSP A/C AFT/FWD GALLEYS , COFFEE MAKERS, AC BAYS, E+E, MAIN GEAR W/W, GALLY OVENS- NO EVIDENCE OF BURNT WIRING NOTED. RMVD AND REPLACED PRI AND AUX BATT CHARGERS, AND PRI AND AUX BATTERIES - OPS CK GOOD . SMELL DISSIPATED. NO HISTORY NOTED. REF B737-700 AFIM 05-51 TASK 814, CONDITIONAL INSP SMOKE OR FUMES IN CABIN 05-51-56, B737-700 AMM 24-31-11, 24-31-31, 24-31-21.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,415 hrs · 34,230 cycles

F/A REPORTS L1 DOOR HARD TO CLOSE WITH LOUD NOISES COMING FROM THE HINGE AREA. GROUNDED - YES. FOUND UPPER HING ARM OF L1 DOOR TO MAKE CRUNCHING SOUND WHEN CLOSING. FOUND DOOR TO BE SAGGING INDICATED BY WEAR OF TRACK GUIDE AND BALL. LUBRICATED L-1 DOOR MECHANISM'S & COMPONENTS, NOISES ARE NOW GONE & DOOR OPERATES SMOOTHLY REF B737-800 AMM 12-25-11-640-801- & 12-25-1-640-802. ADJUSTED L1 DOOR REF AMM 52-11-00-820-801. L1 DOOR SYSTEM TESTS GOOD REF AMM 52-11-00-700-804.

Part: POWER SUPPLY — NONE (UPPER EMERGENCY) · airframe 66,542 hrs · 33,502 cycles

UPPER EMERGENCY DOOR BRUCE LIGHTING CONNECTORS ARE DAMAGED/DETACHED. GROUNDED - YES. REMOVED AND REPLACED UPPER EMERGENCY DOOR LIGHT ASSY AND BATTERY PACK POWER SUPPLY S/N 8226 AND OPS CHECKS GOOD IAW B737-700 AMM 33-21-00-960-897, 33-51-06-960-806, 33-20-00-710-801-001.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 827 IS CRACKED BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 827 BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKE IAW ASA T/C AD20090102-700-25-1R.

Part: FLOOR SUPPORT — CRACKED · airframe 66,542 hrs · 33,502 cycles

R/H FLOOR SUPPORT AT STA 294-328 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED THE CRACKED R/H FLOOR SUPPORT AT STA 294-328 IAW B737-700 SRM 51-40-02-0G-0.

Part: NONE — CORRODED · corrosion level 2 · airframe 66,542 hrs · 33,502 cycles

AFT PIT L/H TRANSITION HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. FOUND TO BE OUT OF LIMITS DUE TO WO: MAT LOSS REMOVED & REPLACED TRANSITION PANEL IAW B737 SRM 53-00-53-2R-5W=3.0 O=.040 R=.000 L=17.0 D=.040.

Part: CARGO TRACK — CORRODED · corrosion level 2 · airframe 66,542 hrs · 33,502 cycles

AFT PIT CARGO TRACK HAS SPOTS OF CORROSION AT STA 787-847. GROUNDED - YES. REMOVED CORROSION ON AFT PIT CARGO TRACK RH OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2 REPAIRED TRACK FROM STA 767-867 IAW B737-700 SRM 53-00-53-2R-3. W=1.0" O=.080" R=.063" L=22" D=.017"

Part: NONE — CORRODED · corrosion level 2 · airframe 66,542 hrs · 33,502 cycles

AFT PIT R/H TRANSITION FROM CARGO DOOR FWD HAS SPOTS OF CORROSION. GROUNDED - YES. FOUND TO BE OUT OF LIMITS DUE TO 100% MAT LOSS REMOVED AND REPLACED TRANSITIONAL PANEL IAW B737 SRM 53-00-53-2R-5W=3.0 O=.040 R=.000 L=17.0 D=.040.

Part: WEB — CORRODED · corrosion level 2 · airframe 66,542 hrs · 33,502 cycles

AFT CARGO DOOR LOWER WEB HAS CORROSION. GROUNDED - YES. AFT CARGO DOOR OUT OF LIMITS IAW 737-700 SRM 53-00-53-1A-2. REMOVED AND REPLAED WEB IAW 737-700 SRM 51-40-02-0G-0W= 1" O= .045" R= .039" L= 4" D= .004".

Part: CARGO TRACK — CRACKED · airframe 66,542 hrs · 33,502 cycles

AFT PIT R/H CARGO TRACK IS CRACKED AT STA 727B AND 727E. GROUNDED - YES. REPAIRED AFT PIT RH CARGO TRACK FROM STA 727 TO 767 IAW B737-700 SRM 53-00-53-2R-3.

Part: SHIELD — CORRODED · airframe 66,542 hrs · 33,502 cycles

FWD PIT R/H SIDE SHEILD AFT OF DOOR HAS CORROSION. GROUNDED - YES. REMOVED CORROSION, FOUND SHIELD TO BE OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2. REMOVED AND REPLACED SHIELD IAW B737-700 SRM 51-40-02-0G-0W= 1.0 O= .032 R= .020 L= 2.0 D= .012.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 66,542 hrs · 33,502 cycles

STA 986 FLOOR BEAM HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. REMOVED AND REPLACED STA 986 FLOOR BEAM UPPER CHORD IAW BOEING 737-700 SRM 53-70-51-2R-4W=2.00 O=.150 R=0 L=6.00 D=.150.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 66,542 hrs · 33,502 cycles

L1 FWD GIRT BAR MOUNT AT STA 312 HAS CORROSION. GROUNDED - YES. REMOVED & REPLACED FITTING IAW B737-700 AMM 20-50-11-910-801 DUE TO 100% MAT LOSSW= 1" O= .080 R= 0 L= 1" D= .080.

Part: FLOOR SUPPORT — CRACKED · airframe 66,542 hrs · 33,502 cycles

L/H FLOOR SUPPORT AT STA 328-344 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED THE CRACKED L/H FLOOR SUPPORT AT STA 328-344 IAW B737-700 SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED · airframe 66,542 hrs · 33,502 cycles

FLOOR SUPPORT AT RBL 0 STA 277-294 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED THE CRACKED FLOOR SUPPORT AT RBL 0 STA 277-294 IAW B737-700 SRM 51-40-02-0G-0.

Part: FITTING — CORRODED · corrosion level 2 · airframe 66,542 hrs · 33,502 cycles

L1 AFT GIRT BAR MOUNT AT STA 344 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLAED L/H GIRT BAR FLOOR MOUNT AT STA 344 IAW BOEING 737-700 SRM 51-40-02-0G-0 DUE TO 100% MAT LOSS.W= .75" O= .080" R= 0 L= 1.75" D= .080".

Part: FLOOR SUPPORT — CRACKED · airframe 66,542 hrs · 33,502 cycles

L/H FLOOR SUPPORT AT STA 312-328 CRACKED. GROUNDED - YES. REMOVED AND REPLACED THE CRACKED L/H FLOOR SUPPORT AT STA 312-328 IAW B737-700 SRM 51-40-02-0G-0.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 747 IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 747 BELOW STGR 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 727B IS CRACKED BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 727B BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKE IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 907 IS CRACKED BELOW STRINGER 8R AT THE AIR CONDITIONER SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED STA 907 FRAME IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 520 IS CRACKED BELOW STRINGER 8R AT THE AIR CONDITIONER SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 520 BELOW STRINGER 8R AT THE AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 380 IS CRACKED BELOW STRINGER 8R AT THE AIR CONDITIONER SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 380 BELOW STRINGER 8R AT THE AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 727D IS CRACKED BELOW STRINGER 8R AT THE AIR CONDITIONER SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 727D BELOW STRINGER 8R AT THE AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 500A IS CRACKED BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 500A BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKE IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 867 IS CRACKED BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 867 BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKE IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 787 IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 787 BELOW STGR 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 500A IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 500A BELOW STGR 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 747 IS CRACKED BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 747 BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKE IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 480 IS CRACKED BELOW STRINGER 8R AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 480 BELOW STRING 8R AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 500C IS CRACKED BELOW STRINGER 8R AT THE AIR CONDITIONER SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 500C BELOW STRINGER 8R AT THE AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 827 IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 827 BELOW 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 440 IS CRACKED BELOW STRINGER 8L AT AIRCONDTIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 440 BELOW STGR 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 360 IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 360 BELOW 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 727B IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 727B BELOW STGR 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 907 IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED STA 907 FRAME IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 500C IS CRACKED BELOW STRINGER 8L AT AIR CONDITIONING SUPPORT BRACKET I/B ATTACH FASTENER. GROUNDED - YES. REPAIRED FRAM AT STA 500C BELOW STGR 8L AT AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 66,542 hrs · 33,502 cycles

FRAME AT STA 440 IS CRACKED BELOW STRINGER 8R AT THE AIR CONDITIONER SUPPORT BRACKET I/B FASTENER. GROUNDED - YES. REPAIRED FRAME AT STA 440 BELOW STRINGER 8R AT THE AIR CONDITIONING SUPPORT BRACKET IAW ASA T/C AD20090102-700-25-1R.

Part: TRU — FAILED (E/E BAY) · airframe 65,005 hrs · 32,214 cycles

SMOKE IN FLIGHT DECK AND CABIN FOLLOWED BY ELEC MASTER CAUTION FOR TRU UNIT LIGHT. GROUNDED-YES. NR 3 T/R UNIT CAUGHT FIRE ON RT SIDE OF UNIT, WHICH ALSO DAMAGED NR 2 T/R UNIT. THE LRU TO THE LEFT IS RIGHT FRONT WINDOW HEAT CONTROL UNIT AND WAS ALSO DAMAGED. THE CONNECTOR AT BACK OF RACK WAS NOT DAMAGED. CLEANED RACKS AND FOUND ALL THREE RACKS SERVICEABLE (RACKS FOR NR 2 AND NR 3 T/R UNIT AND RIGHT FRONT WINDOW HEAT CONTROL UNIT). REMOVED AND REPLACED NR 2 AND NR 3 T/R UNITS, IAW B737-700 AMM 24-32-11-000-801 AND 24-32-11-400-801. OPERATIONS CHECK GOOD. REMOVED AND REPLACED RIGHT FRONT WINDOW HEAT CONTROL, IAW AMM 30-41-11-000-801 AND AMM 30-41-11-400-801. OPERATIONS CHECK GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 64,587 hrs · 31,834 cycles

PERFORMING TASK CARD 78233001. LT AND RT AFT GALLEY AND LT AND RT ROWS 19 AND AFT EMERGENCY LIGHTS FAILED 15 MINUTE OPS TEST. GROUNDED - YES. REF TO B737-700 AMM 33-51-06 AND WDM B737-700 33-51-11 FOR WORK ACCOMPLISHED. REMOVED & REPLACED EMERGENCY BATTERY PACKS AT LT & RT POSITIONS AT STA 952, SYSTEM OPS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 62,519 hrs · 29,968 cycles

CENTER WING BOX FRW SPAR UPPER SHEAR TIE AT LBL 15.04 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED CENTER WING BOX FRW SPAR UPPR SHEAR TIE FITTING AT LBL 15.04 IAW 737-700 SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 62,519 hrs · 29,968 cycles

CENTER WING BOX FRW SPAR UPPER SHEAR TIE AT RBL 15.04 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED CENTER WINGBOX FRW SPAR UPPER SHEAR TIE AT RBL 15.04 IAW 737-700 SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 62,519 hrs · 29,968 cycles

CENTER WING BOX FRW SPAR UPPER SHEAR TIE AT RBL 6.14 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED CENTER WING BOX FWD SPAR UPPER SHEAR TIE FITTING AT RBL 6.14 IAW 737-700 SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 62,519 hrs · 29,968 cycles

CENTER WING BOX FRW SPAR UPPER SHEAR TIE AT LBL 6.14 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED CENTER WINGBOX FRW SPAR UPPER SHEAR TIES FITTING AT LBL 6.14 IAW 737-700 SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 62,519 hrs · 29,968 cycles

CENTER WING BOX FRW SPAR UPPER SHEAR TIE AT RBL 32.40 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED CENTER WINGBOX FRW SPAR UPPER SHEAR TIE AT RBL 32.40 IAW 737-700 SRM 51-40-02-0G-0.

Part: LENS — DETACHED (EXIT SIGN) · airframe 62,190 hrs · 29,695 cycles

LENS WILL NOT STAY ON R-2 DOOR. EXIT SIGN NEXT TO DOOR. GROUNDED - YES. REPLACED R2 DOOR EXIT SIGN IN REF TO AMM 33-51-01.

Part: LATCH — DEFECTIVE (EVAC SLIDE) · airframe 60,577 hrs · 28,367 cycles

SLIDE L1 DOOR DETACHED. GROUNDED - YES. REMOVED L1 DOOR SLIDE PACK. REMOVED AND REPLACED SLIDE PACK LATCH. REINSTALLED L1 DOOR SLIDE PACK ASSY REF AMM 25-66-01.

Part: MUFFLER — DISCONNECTED (AIR DISTRIBUTION) · airframe 59,069 hrs · 27,098 cycles

SUPPLY DUCT TEMP BECAME VERY HOT AND UNCONTROLLABLE WITH AUTO AND MANUAL CONTROL. CABIN BECAME VERY HOT AND DISCHARGE LIGHT ILLUMINATED ON CENTER CONSOLE. FIRE RESPONSE FOUND NORMAL HEATING AND NOTHING UNUSUAL FOUND WHEN CARGO DOORS OPENED. DISCHARGE LIGHT WENT OUT WHILE THE CREW WAS RESPONDING. ACFT GROUNDED. EMERGENCY DECLARED . REMOVED LINING AT AFT END FWD CARGO COMPARTMENT, FOUND MUFFLER ASSY DISCONNECTED. CHECKED CARGO DISCHARGE PRESSURE SWITCH IAW WDM 26-23-11. NO DEFECT NOTED. REPLACED THE MUFFLER AND REASSEMBLED DUCT ASSEMBLY. OPS AND LEAK CHECKED GOOD.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 58,418 hrs · 26,614 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO R-2 DOOR HAS DAMAGED LENS. ACFT GROUNDED. REPLACED THE LENS AND TESTED THE LIGHT ASSY IAW AMM 33-51-01-960-801. OPS NORMAL.

Part: WINDOW FRAME — CRACKED (BS 224) · airframe 58,102 hrs · 26,377 cycles

R3 WINDOW POST IS CRACKED AT THE SECOND LOWER FASTENER HOLE. ACFT GROUNDED REPAIRED.

Part: WINDOW FRAME — CRACKED (BS 211) · airframe 58,102 hrs · 26,377 cycles

R1 WINDOW POST IS CRACKED IN RADIUS OF UPPER CORNER. ACFT GROUNDED. REPAIRED THE WINDOW FRAME.

Part: BOLT — BROKEN (R1 DOOR) · airframe 57,738 hrs · 26,161 cycles

R1 DOOR WILL NOT CLOSE. GROUNDED - YES. FOUND BOLT BROKEN IN UPPER LINK ASSY, REPLACED BOLT AND LUBED DOOR REF AMM 52-41-00. NO ADJUSTMENT NEEDED. OPS NORMAL.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 56,937 hrs · 25,688 cycles

FA REPORTS L1 DOOR DIFFICULT TO OPEN. GROUNDED - YES. FOUND GUIDE ARM OUT OF ADJUSTMENT ADJUSTED GUIDE ARM REF AMM 52-11-00-820-801 STEP 2H(1) CHECKED HANDLE FORCE, HANDLE FORCE AND FLIGHT DECK LIGHTS CHECKED GOOD REF AMM 52-11-00-700-804.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 56,052 hrs · 25,293 cycles

EMERGENCY LIGHT EXIT SIGN LENS FALLING OFF OF LIGHT ASSY AT L-2 DOOR. ACFT GROUNDED. REMOVED AND REPLACED THE LENS AND TESTED LIGHT ASSY IAW AMM 33-51-01-960-801 - OPS NORMAL.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 55,792 hrs · 25,176 cycles

EXIT SIGN FOR L2 DOOR MISSING. ACFT GROUNDED. REPLACED MISSING EXIT SIGN FOR L2 DOOR.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 53,277 hrs · 24,015 cycles

FWD ENTRY DOOR L1- OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP L1 SLIDE LIGHT AND PERFORMED GOOD LAMP TEST IAW AMM 33-51-04-960-801.

Part: FLOOR PANEL — DAMAGED (BS 947) · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN FLOOR PANEL, PN 147A5810-18 HAS 2 EA. INSERTS THAT REQUIRE RELOCATION, FLOOR BEAM REPAIR, BS 947-BS 947, WL 208-WL 208. ACFT GROUNDED. REPAIRED PANEL AND RELOCATED INSERTS IAW REO -G19374, REV B ATTACHED TO G599043 AND EA 700-53EA-16190.

Part: SKATE ANGLE — CHAFED (BS 1017-1133) · airframe 53,277 hrs · 24,015 cycles

VERTICAL STABILIZER PANELS 323BL, 323CL,AND 324AL LOWER SUPPORT ANGLE HAS CHAFING MARKS BETWEEN BS 1017 AND BS 1138, STR 2L AND 3L . ACFT GROUNDED. BLENDED AREA IAW SRM 51-10-02 & EA NG-55EA-03820, REV NEW FOUND TO BE OUT OF LIMITS AT BS 1124, ORIG .063 REMAINING .046, REMOVED .017, TOOL T8225Y CAL DUE 12-03-2015. REMOVED PANEL 324QL IAW AMM 55-33-31. REPAIRED IAW EA NG-55EA-03820, REV NEW INSTALLED PANEL 324QL IAW AMM 55-33-31 REMOVED DOT .

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 53,277 hrs · 24,015 cycles

CABIN FLOOR PANEL 222BF DELAMINATED, PN 141A5810-176, PARTS RACK. ACFT GROUNDED. REMOVED INSERTS FOR REPAIR, REMOVED DAMAGED PLIES, FABRICATED REPAIR PLIES LAYED UP REPAIR VACUUM BAGGED AND CURED IAW REO-G19374, REV B AND SRM 53-00-50-2R-0, REO G19374 REV B ATTACHED TO G599043 AND EA 700-53EA-16190.

Part: DOOR FRAME — CRACKED (BS 291-303) · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN R-1 DOOR SURROUND WEB FORWARD LOWER CORNER CRACKED. ACFT GROUNDED. R & R 141A8371-8, FRAME AND 141A8372-2 DEPRESSOR IAW SRM 51-40-02 AND BAC DWG 141A8371, REV "A". AERO-SMOOTHER WILL BE APPLIED ON JC N4253000.

Part: SKIN — CORRODED (BS 984) · airframe 53,277 hrs · 24,015 cycles

AREA OF AFT CARGO COMPARTMENT SKIN HAS CORROSION AT BS 984 BETWEEN STR 19R AND STR 20R. ACFT GROUNDED. REMOVED CORROSION FROM SKIN DOUBLER. ORIGINAL MATERIAL 0.056" REMOVED .003" REMAINING MAT .053". FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01 AND DWG 147A3424. ALODINE AND PRIME IAW SRM 51-20-01 AND SOPM 20-41-02. INSTALLED FASTENER IAW ACTUATER REMOVAL IAW SRM 51-40-02. APPLIED TOP COAT IAW SOPM 20-41-02. IDENTIFIED CORROSION BLEND OUT AREA IAW AMM 51-05-01-701. APPLIED CIC IAW AMM 51-21-01. REMOVED DOT: W466.

Part: SUPPORT — CORRODED (BS 727D) · airframe 53,277 hrs · 24,015 cycles

AFT CARGO PIT LT SIDEWALL PANEL SUPPORT HAS LIGHT CORROSION AROUND HOLE AT BS 727D BETWEEN STR24L AND STR25L. ACFT GROUNDED. ORIGINAL .063, REMOVED .004, REMAINING MATERIAL .059, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-07-1A-1. ALODINED AND PRIMED IAW SRM 51-20-01-0G-0. REMOVED DOT.

Part: TRANSITION PANEL — CORRODED (BS 500B-500D) · airframe 53,277 hrs · 24,015 cycles

FWD CARGO BAY LT SIDE TRANSITION PANEL CORRODED FROM LT BS 500B TO FWD PIT AFT BULKHEAD. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, WITHIN LIMITS IAW SRM 53-00-53, FIG 103. ORIGINAL THICKNESS 0.040 WITH 0.038, REMAINING 0.002 MATERIAL REMOVED MEASURED WITH UT GAUGE T8225P, ALODINED AND PRIMED IAW SRM 51-20-01.

Part: FLOORBEAM — CORRODED (B 772) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE, TEE STRAP AT BS772 HAS CORROSION IN SEVERAL AREAS, MARKED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. BEYOND LIMITS IAW SRM 53-00-53, FIG 103. ORIGINAL THICKNESS WAS 0.070 WITH 0.040 REMAINING, 0.030 MATERIAL REMOVED. RECEIVED A NEW FLOOR PANEL SPLICE SUPPORT STRAP; TO BE INSTALLED ON OP 9900. PO 852057.1, REMOVED DOT.

Part: BRACKET — CORRODED (BS 500-500A) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

FWD PIT AFT BILGE ANTENNA BRACKET IS CORR AT STA 500 TO STA 500A. ACFT GROUNDED. REMOVED NR 1 ANTENNA BLANKING PLATE IAW AMM 23-19-07. REMOVED ANTENNA BRACKETS IAW SRM 51-40-02, MATERIAL ID 7075-T6, .040, PO 804411.4 AND FABBED IAW DWG 143A3233, REV F LOCATED AND DRILLED IAW SRM 51-40-05 TREATED IAW SOPM 20-43-03 AND SRM 51-20-01 INSTALLED BRACKETS IAW SRM 51-40-02 INSTALLED BLANKING PLATE IAW AMM 23-20-02. REMOVED DOT.

Part: TRANSITION PANEL — CORRODED (BS 727C-787) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE LT TRANSITION PANEL FROM BS 736 TO BS 787 HAS CORROSION, MARKED. ACFT GROUNDED. CUTOUT DAMAGE PORTION OF AFT CARGO LT TRANSTION PANEL, FABRICATED, LOCATED & DRILLED NEW REPAIR PARTS USING BAC 1496-377 EXTRUSION PO 843790.6, APPLIED ALODINE, PRIME & TOPCOAT TO REPAIR PARTS & REPAIR AREA, INSTALLED ALL REPAIR PARTS & APPLIED CIC TO REPAIR AREA,ALL WORK PERFORMED IAW SRM 53-00-3-2R-6 REMOVED MAINT DOT U843.

Part: TRANSITION PANEL — CORRODED (BS 767-787) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE RT TRANSITION PANEL FROM BS 767 TO BS 787 HAS CORROSION, MARKED. ACFT GROUNDED. REMOVED CORROSION ON SHIELD, TRANSITION PANEL FROM BS 767 TO BS 787 IAW SRM 51-10-02. ORIGINAL THICKNESS IS .050. REMOVED DOT REMAINING THICKNESS IS .043. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 AND SRM 53-60-53. R & R SHIELD IAW SRM 51-40-02 & DWG 146A8127, REV C DOT REMOVED.

Part: BRACKET — CORRODED (BS 500A-500B) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

FWD PIT AFT BILGE ANTENNA BRACKET IS CORRODED AT BS 500A TO 500B. ACFT GROUNDED. REMOVED NR 2 ANTENNA BLANKING PLATE IAW AMM 23-19-07. REMOVED ANTENNA BRACKETS IAW SRM 51-40-02, MATERIAL ID 7075-T6 .040, PO 804411.4 AND FABBED IAW BAC DWG 143A3233, REV F. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED IAW SOPM 20-43-03 AND SRM 51-20-01. INSTALLED BRACKETS IAW SRM 51-40-02. INSTALLED BLANKING PLATE IAW AMM 23-20-02, REMOVED DOT.

Part: WEB — CORRODED (BS 440-492) · airframe 53,277 hrs · 24,015 cycles

FWD CARGO THRESHOLD IS CORRODED. ACFT GROUNDED. ORIGINAL MATERIAL .045", REMOVED .001", REMAINING MATERIAL .044; FOUND TO BE WITHIN LIMITS IAW SRM 53-30-15-1A-1, PAGE 7, FIG 103. APPLIED ALODINE AND PRIMER IAW SRM 51-20-01-OG-0.

Part: FLOOR SUPPORT — CORRODED (BS 727-727A) · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE AT BS 727 AND BS 727A AND LBL 12.5 HAS CORROSION. MARKED. ACFT GROUNDED. BLEND OUT CORROSION AREA, ORIGINAL MATERIAL THICKNESS .063 IAW DWG 1509-100146, MAT REMOVED .004, MAT REMAINING .059, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2, ALODINE AND PRIMER IAW SRM 51-20-01, DOT V841, REMOVED.

Part: FLOOR SUPPORT — CORRODED (BS 787-793) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT, FLOOR SUPPORT/TRANSITION PANEL BETWEEN BS787 TO BS793 AND S26R & S25R HAS CORROSION ON UPPER AND LOWER SURFACE, MARKED. ACFT GROUNDED. REMOVED CORROSION FROM TOP AND BOTTOM FLOOR SUPPORT STRAPS AT BS 787-793, 526R-25R IAW SRM 53-00-83 -1A, ORIGINAL THICKNESS OF TOP STRAP IS .100 IAW SRM 53-60-15, FIG 5, TABLE 4, REMAINING THICKNESS .086, REMOVED .014, TOP STRAP OUT OF LIMITS IAW SRM 53-00-53-1A, FIG 103 DET D,ORIG THICKNESS OF BOTTOM STRAP IS .170 IAW BAC 146A8128 REV B, REMAINING THICKNESS .118. REMOVED .052,BOTTOM STRAP IS OUT OF LIMITS IAW SRM 53-00-53-1A, FIG 103, DET D, REMOVED OLD STRAPS AND INSTALLED NEWSTRAPS, PN 146A8128U1, PO 852290.5 AND 146A8128-2, PO 852290.5 IAW SRM 51-40-02, DOT REMOVED IAW BAC 146A8120, REV E.

Part: SEAT TRACK — CORRODED (BS 767-887) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE, TRACK AT BS 792 AND RBL 13.84 HAS CORROSION. MARKED. ACFT GROUNDED. R & R WITH NEW AFT CARGO COMPARTMENT FLOOR STRUCTURE TRACK IAW SRM 53-00-53-2R-3 & BAC DWG 146A7501, REV:C REMOVED DOT U847.

Part: DOOR SILL — CORRODED (BS 793-847) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT, DOOR SILL AREA HAS CORROSION IN SEVERAL AREAS FROM BS 793 TO BS847, MARKED. ACFT GROUNDED. UPON FURTHER INVESTIGATION OF AFT CARGO DOOR LOWER SILL, MAIN TO BE .045 ORIGINAL THICKNESS, MATERIAL REMOVED IS .006. REMAINING THICKNESS .039 WHICH IS OUT OF ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1, SECTION 4, PARAGRAPH G, STEP 2 & SRM 53-60-15-0I-1 FOR IDENTIFICATION TOOL T8225Z, UT GAUGE. REMOVED DOOR SILL WEB IAW SRM 51-40-02. FABRICATED NEW DOOR SILL WEB IAW DWG 146A8123, REV F ALODINE TREATED AND APPLIED PRIMER TO NEW SILL WEB IAW AMM 51-21-41 AND 51-21-72. INSTALLED NEW SILL WEB IAW SRM 51-40-02. REMOVED DOT.

Part: FLOOR SUPPORT — CORRODED (BS 727-727A) · airframe 53,277 hrs · 24,015 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE AT BS 727 AND BS 727A AND RBL 13.84 HAS CORROSION. MARKED. ACFT GROUNDED. BLEND OUT AREA ORIGINAL MATERIAL THICKNESS, .063 IAW DWG 1509-100146, MAT REMOVED .001 MAT REMAINING .062 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2, ALODINE AND PRIMER IAW SRM 51-20-01, DOT V840 REMOVED.

Part: GIRT BAR — CORRODED (BS 344-346) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN GIRT BAR ATTACH FLOOR FITTING CORRODED BS 344-BS 346, LBL 58-LBL 60. GROUNDED. R & R 141A5220-4, TIE DOWN FITTING IAW SRM 51-40-02. DOT REMOVED.

Part: FLOOR SUPPORT — CORRODED (BS 987-993) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT FUSELAGE WET AREA, BS 987 +6, LBL 40 HAS CORROSION. ACFT GROUNDED. ORIGINAL MATERIAL THICKNESS .050", DAMAGED MATERIAL THICKNESS .007, REMAINING MATERIAL THICKNESS .043", FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51USING UT GAUGE TOOL T8225Z, REMOVED SUPPORT BRACKET IAW SRM 51-40-02, RECEIVED NEW SUPPORT BRACKET PN 147A5710Y1. LOCATED, REAMED AND COUNTERSANK FASTENER HOLES ON NEW SUPPORT BRACKET IAW SRM 51-40-08, INSTALLED NEW SUPPORT BRACKET IAW SRM 51-40-02, DOT REMOVED .

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT FUSELAGE WET AREA STA 947.5 RBL 49 HAS CORROSION. ACFT GROUNDED. AFT FUSELAGE WET AREA BS 947.5 TOP OF THE FLOORBEAM CHORD CORRODED BEYOND LIMITS IAW SRM 53-70-51. REMOVED DAMAGE AND REPAIRED CHORD IAW SRM 53-70-51-2R-5, SRM 51-10-02, SRM 51-40-02, SRM 51-40-05, SRM 51-20-01, SOPM 20-10-03, SOPM 20-41-02. APPLIED CIC IAW SRM 51-20-01. DOT REMOVED.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN FLOORBEAM BS 344, REPAIR HAS CORROSION, LBL 5. ACFT GROUNDED. REPAIRED FLOORBEAM REF: REO-G19363, REV B AND EA 700-53EA-16186, REV NEW, DOT REMOVED.

Part: SUPPORT — CORRODED (BS 992-1016) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT FUSELAGE WET AREA, BS 1016, LBL 32 HAS CORROSION AND BENT. ACFT GROUNDED. REMOVED CORRODED AND BENT WALL SUPPORT, RECEIVED NEW WALL SUPPORT, PN 147A5710U16, LOCATED, DRILLED AND COUNTERSANK FASTENER HOLES ON NEW WALL BRACKET IAW SRM 51-40-08, INSTALLED NEW WALL SUPPORT IAW SRM 51-40-02, DOT REMOVED.

Part: FLOOR SUPPORT — CRACKED (BS 318-328) · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN BELOW FLOOR SUPPORT CRACKED BS 320, LBL 46. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5910, REV U.

Part: FLOOR SUPPORT — CORRODED (BS 992-1016) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT FUSELAGE WET AREA, BS 1006, RBL 31 HAS CORROSION. ACFT GROUNDED. REMOVED FLOOR SUPPORT IAW SRM 51-40-02. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .050 MATERAIL LOSS .008, MATERIAL REMAINING .042" FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51, LOCATED AND DRILLED NEW SUPPORT, PN 147A5710U17 AND INSTALLED IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 637-641) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN, FLOOR SUPPORT CORRODED BS 637-BS 641, RBL 62-RBL 65. ACFT GROUNDED. REPAIRED IAW EA 700-53, EA-16116 AND REO-G19342, REV A DOT REMOVED.

Part: FLOOR SUPPORT — CRACKED (BS 320-344) · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN BELOW FLOOR SUPPORT CRACKED BS 334, LBL 46. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5410, REV U.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN RT FLOORBEAM BS 328 CORROSION ON UPPER SURFACE. ACFT GROUNDED. REPAIRED FLOORBEAM BS 328, RBL40-RBL65 IAW SRM 53-10-51-2R-7.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN GIRT BAR ATTACH FLOOR FITTING CORRODED BS 308-BS 310, LBL 58-LBL 60. ACFT GROUNDED. R & R 141A5220-2 TIE DOWN FITTING IAW SRM 51-40-02. DOT REMOVED.

Part: FLOOR SUPPORT — CORRODED (BS 259-360) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT R-1 DOOR AREA. ACFT GROUNDED. R & R R-1 DOOR CHORD, PN 654A0004-134 IAW AND REF DWG'S 141A8310, 143A5900, 140A9810. DOT REMOVED.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN RT FLOOR SUPPORT BETWEEN BS 312 - 328 IS CRACKED RBL 33. ACFT GROUNDED. REMOVED THE CRACKED INTERCOSTAL IAW SRM 51-40-02. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02.

Part: ANGLE — CHAFED (BS 1005-1009) · airframe 53,277 hrs · 24,015 cycles

VERTICAL STABILIZER PANEL 323AL, LOWER SUPPORT ANGLE HAS CHAFING MARKS BETWEEN BS 1005 AND BS 1016 ,STR 2L AND 3L. ACFT GROUNDED. BLENDED AREA IAW SRM 51-10-02 & EA NG-55-EA-03820, REV NEW FOUND TO BE OUT LIMITS AT BS 1005 ORIGINAL .063 REMOVED .011 REMAINING .052 TOOL, T8225Y CAL DUE 12-03-2015. REPAIRED IAW EA NG-55EA-03820, REV NEW REMOVED DOT.

Part: STRINGER — DENTED (BS 360) · airframe 53,277 hrs · 24,015 cycles

MAIN CABIN BS 360 S9-R, STRINGER SPLICE IS BENT. ACFT GROUNDED. R & R STRINGER CHANNEL AND STRINGER CLIP REF: SRM 51-40-02 AND BAC DWG 140A9111, REV B. REMOVED DOT.

Part: SUPPORT ANGLE — BENT (L2 DOOR) · airframe 53,277 hrs · 24,015 cycles

L2 DOOR SCUFF PLATE SUPPORT ANGLE BENT. ACFT GROUNDED. REMOVED BENT SUPPORT ANGLE IAW SRM 51-40-02. RECEIVED MATERIAL ID SUPPORT ZEE BAC 1517-2797-7075-T73511 EXTRUSION TO FABRICATE NEW SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE IAW DWG 147A8530 AND GPM 05-00-85. APPLIED ALODINE IAW AMM 51-21-41. APPLIED PRIMER IAW AMM 51-21-72. INSTALLED L2 DOOR SCUFF PLATE SUPPORT ANGLE IAW SRM 51-40-02. DOT REMOVED.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,277 hrs · 24,015 cycles

CRACK FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN JUST INBD OF STABILIZER STATION 92.70. CRACK IS APPROXIMATELY .5" LONG AND APPROXIMATELY 10" FWD OF DRAIN HOLE AND IS MARKED. ACFT GROUNDED. REPAIRED LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT BS 92.70 IAW SRM 55-10-01-2R-11. INSPECTION THRESHOLD 56,000 CYCLES AFTER REPAIR INSTALLATION METHOD: DETAIL VISUAL INSPECTION AND EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION INTERVAL, 9000 FLIGHT CYCLES TABLE 204. .

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,277 hrs · 24,015 cycles

CRACK FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN JUST INBD OF STABILIZER BS 101.90. CRACK IS APPROXIMATELY .5" LONG AND APPROXIMATELY 10 AFT OF DRAIN HOLE AND IS MARKED. ACFT GROUNDED. REPAIRED LOWER SKIN OF RT HORIZONTAL STABILIZER AT BS 101.90 IAW SRM 55-10-01-2R-11. INSPECTION THRESHOLD 5600 CYCLES AFTER REPAIR INSTALLATION METHOD. DETAIL VISUAL INSPECTION AND EXTERNAL LOW FREQUENCY EDDY CURRENT INSEPCTION INTERVAL: 9000 FLIGHT CYCLES.

Part: SUPPORT — WORN (PYLON) · airframe 53,277 hrs · 24,015 cycles

RIGHT WING T/E OTBD OF PYLON, SUPPORT ROD ATTACH BRACKET HOLES WORN. ACFT GROUNDED. R & R BRACKET IAW SRM 51-40-02 AND BAC DWG 115A6400, LEAK CHECK ACCOMPLISHED ON TASK CARD 74528002, DOT REMOVED.

Part: SHIM — MIGRATED (BS 663) · airframe 53,277 hrs · 24,015 cycles

WING AFT SPAR LOWER ATTACH FITTING BL71.24 LT BS 663.75 HAS TORN SEALANT AND MIGRATING SHIMS. ACFT GROUNDED. REPAIRED IAW REO-G19315 A REQUIRES INSPECTION: "INSPECT THE JOINT FOR BOLT/NUT ROTATION OR ADDITIONAL SHIM MIGRATION WITH IN 200 CYCLES OR 12 MONTHS, WHICHEVER COMES FIRST FROM 11/06/2015. CONTACT ENGINEERING IF ANY FINDING IS FOUND. PROVIDED THAT THERE IS NO FURTHER SHIM MIGRATION AND BOLT/NUT ROTATION AS A RESULT OF THE ABOVE SUPPLEMENTAL INSPECTION, THE REPAIR ACCOMPLISHED IAW EA 700-57 EA-16102 IS CONSIDERED A PERMANENT REPAIR." DOT REMOVED .

Part: FLOOR PANEL — CORRODED (BS 727D-767) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT PIT FLOOR PANEL 140BF HAS CORROSION AND GOUGES ALL ARROUND. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL 140BF IAW DWG 453A2610, REV E.

Part: FLOOR PANEL — DAMAGED (BS 887-947) · airframe 53,277 hrs · 24,015 cycles

AFT CARGO BAY FLOOR PANEL 140DF HAS CORROSION AND GOUGES ALL ARROUND. ACFT GROUNDED. EVALUATED DAMAGE ON FLOOR PANEL 140DF, FOUND OUT OF LIMIT ACCORDING TO SRM 53-00-53, MATERIAL ID TO FABRICATE NEW PANEL 2024-T3 .071" IAW B-DWG 453A2610, PO:8406181.1. FABRICATED PANEL IAW B-DWG 453A2610, SRM 53-00-53-1A-1, REV 26. ALODINED AND APPLIED PRIMER IAW SRM 51-20-01-0G-0, DOT REMOVED.

Part: FLOOR PANEL — CORRODED (BS 727-767) · airframe 53,277 hrs · 24,015 cycles

AFT PIT FLOOR PANEL 140AF HAS CORROSIN AND GOUGES ALL ARROUND. ACFT GROUNDED. EVALUATE DAMAGE ON AFT PIT FLOOR PANEL 140AF FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 REV 26, FABRICATED NEW FLOOR PANEL IAW DWG 453A2610, THE NEW PANEL WAS ALODINED AND PRIMED IAW SRM 51-20-01.

Part: FLOOR PANEL — CORRODED (BS 767-887) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT PIT FLOOR PANEL 140CF HAS CORROSIN AND GOUGES ALL ARROUND. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL 140 CF IAW DWG 453A2610, FLOOR PANEL 140CF HAS MULTIPLE GOUGES LINGER THAN 3", PN 453A2610, FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1.

Part: FLOOR PANEL — CORRODED (BS 440-500) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

PARTS RACK, FWD PIT FLOOR PANEL 120BF CORRODED AND GOUGED IN SEVERAL AREAS. ACFT GROUNDED. FLOOR PANEL NR 120BF, PN 453A1610-44 HAS MULTIPLE GOUGES LONGER THAN 3". FOUNT TO BE OUT OF LIMITS PER ASA B737-700 SRM 53-00-53-1A-1. FABRICATED NEW FLOOR PANEL, PO 851953.2 IAW DWG 453A1610, REV: T. ALODINED IAW SOPM 20-41-02 AND PRIMED LOWER SURFACE IAW AMM 51-21-72. DOT REMOVED.

Part: STRIP — CORRODED (SIDEWALL PANEL) · corrosion level 2 · airframe 53,277 hrs · 24,015 cycles

AFT CARGO RT SIDEWALL CAPSTRIP NR 2 CORRODED. ACFT GROUNDED. RECEIVED NEW CAP STRIP PN 453A2611-11. INSTALLATION ACCOMPLISHED.

Part: FLOOR PANEL — CORRODED (BS 400-440) · airframe 53,277 hrs · 24,015 cycles

PARTS RACK, FWD PIT FLOOR PANEL 120AF CORRODED SEVERAL AREAS. ACFT GROUNDED. BLENDED OUT PANEL 120AF ORIGINAL MATERIAL .071, MATERIAL REMOVED IS .020 MATERIAL REMAINING IS .051 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED NEW FLOOR PANEL IAW DWG 453A1610, REV:E. ALODINED IAW SRM 51-20-01 AND PRIMED IAW DWG 453A1610 REV: T AND AMM 51-21-72.

Part: TRACK — GOUGED (BS 727-767) · airframe 51,994 hrs · 23,394 cycles

RT ZEE TRACK AT ST 749 TO HAVE A .2500" PUNCTURE. ACFT GROUNDED. REPAIRED RT TRANSITION PANEL IN AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-5 FROM STA 727-STA 767.

Part: MODULE — CORRODED (CABIN) · airframe 51,327 hrs · 23,049 cycles

WHILE PERFORMING TC 78233008, EMERGENCY LIGHT CK FOUND LIGHT AT 20D DIM AND ALWAYS ON. ACFT GROUNDED. GROUND MODULE GD03806 CORRODED. REPLACED GROUND MODULE IAW SRM 51-40-02. RE-TERMINATED W4142-0455-20, W4146-0072-18, AND W4146-0073-18 AND INSTALLED WIRES INTO GD 03806, REF SWPM 20-90-15. OPS TEST OF EMERGENCY LIGHTS AND CEILING LIGHTS OK REF AMM 33-51-00-710-801 & 33-20-00-710-801-001.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 51,311 hrs · 23,043 cycles

FOUND L1 DOOR HARD TO LATCH WHILE INSIDE, END OF TRAVEL. ACFT GROUNDED. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED L-1 DOOR GUIDE ARM REF AMM 52-11-00-820-801 STEP H. ACCOMPLISHED FORWARD ENTRY DOOR SYS TEST & TESTED GOOD REF AMM 52-11-00-700-804.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 50,828 hrs · 22,829 cycles

BULL NOSE EMERGENCY LIGHT AT ROW 20 FED & 21 FED WILL NOT GO OUT. ACFT GROUNDED. REPLACED BATTERY PACK/CHARGER M1672 AND RELAMPED L1065 AISLE LIGHT BETWEEN ROWS 20 AND 21 FED. OPS CHECK OK, REF AMM 33-51-06/201.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,312 hrs · 22,580 cycles

EMERGENCY LIGHT OVERWING EXIT HANDLE, FLOODLIGHTS AT LT AND RT OVERWING EXITS EACH HAVE BOTH LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.

Part: SCREW — LOOSE (COCKPIT WINDOW) · airframe 48,557 hrs · 21,749 cycles

CAPTAIN`S SLIDING WINDOW WILL NOT FULLY OPEN. ACFT GROUNDED. INSPECTED WINDOW IAW MM 56-12-11-710-803. TIGHTENED ONE SCREW ON AFT WINDOW SHADE SLIDE RAIL. OPS CHECKED NORMAL. NO REPAIRS, RIGGING OR ADJUSTMENTS WERE REQUIRED.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 47,311 hrs · 21,169 cycles

SEAT TRACK BS 727B, RBL 45.50 CRACKED. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G16843, REV B AND EA 700-53EA-11540, REV.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 47,311 hrs · 21,169 cycles

SEAT TRACK AT BS 727B, RBL 24.75 CRACKED. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G16843, REV B AND EA 700-53EA-11540, REV.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 46,831 hrs · 20,953 cycles

CLIMBING THOUGH 17,000 FT, NR 2 ENGINE SURGED CONTINUALLY. RAN SURGE CHECKLIST, THROTTLE ALMOST CLOSE WHEN ENGINE STALLED, ENGINE THEN FAILED. COMPLETED CHECKLIST AND RETURNED DEPARTURE. ACFT GROUNDED. ACCOMPLISHED EA 700-72EA-10951. NR 2 ENGINE HMU REPLACED. REV B. ITEMS ACCOMPLISHED ON REV B ARE TO BE ATTACHED TO EA 700-72 EA-10951 REV C, ITEM 15, ON REV C WAS ACCOMPLISHED ON REV B, ITEMS 1-14 ON EA 700-72EA-10951, REV C COMPLETED ON REV B, EA 700-72EA-10951.

Part: GUIDE ARM — OUT OF ALIGNMENT (L1 DOOR) · airframe 44,261 hrs · 19,769 cycles

ACFT L1 DOOR DID NOT CLOSE AND LOCK PROPERLY CAUSING AN AIR LEAK AND LACK OF PROPER PRESSURIZATION. NO LIGHT CAME ON IN FLIGHT OR GROUND. ACFT GROUNDED. FOUND L1 DOOR OUT OF ALIGNMENT WITH FUSELAGE SKIN. ADJUSTED GUIDE ARM IAW AMM 52-17-00-820-801, STEP 2 A-H. ACCOMPLISHED GVI OF DOOR LATCH MECHANISM, CONTROL RODS AND UPPER AND LOWER GATES. NO DEFECTS NOTED. PRESSURIZED ACFT TO 4 PSIG IAW MANUAL MODE TEST AMM 21-31-00. NO LEAKS NOTED. PRESSURIZATION NORMAL.

Part: WINDOW POST — CRACKED (BS 196-200) · airframe 44,179 hrs · 19,733 cycles

CRACK ON LT NR 1 WINDOW OTBD POST. ACFT GROUNDED. REPAIRED IAW SB737-53-1336-NG-1.

Part: BULKHEAD — CRACKED (BS 663) · airframe 44,179 hrs · 19,733 cycles

WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK HAS A CRACK STA 663, RBL 43 5. BELOW THE PRESSURE WEB. ACFT GROUNDED. INVESTIGATED CRACK ON WING CENTER SECTION REAR SPAR VERTCAL PRESSURE DECK WEB CRACK. FOUND TO BE 3 LONG AND OUT OF LIMITS BS663, RBL 43.5 BELOW PRESSURE WEB. REMOVED DAMAGED SECTION RBL 32-48.5 FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-10-10, REPAIR 3, ALTERNATIVE 2.

Part: WINDOW FRAME — CRACKED (BS 221) · airframe 44,179 hrs · 19,733 cycles

POSSIBLE CRACK ON LT NR 1 WINDOW OTBD POST. REPAIRED CRACK ON NR 1 WINDOW POST BY FABRICATING AND INSTALLING EXTERNAL DOUBLER IAW EA 700-53EA-09202.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,172 hrs · 18,329 cycles

NUT PLATE SPLICE STRIP CORRODED. REPLACED SPLICE STRIP.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,172 hrs · 18,329 cycles

AFT CARGO COMPARTMENT AFT BULKHEAD ATTACH ANGLE CORRODED BS 947 LBL 22 RBL 22. REMOVED CORROSION AND CHECKED LIMITS ORIGINAL THICKNESS .080 REMAINING IS .065 .015 WAS REMOVED. FOUND TO BE OUT OF LIMITS REF B737 700 SRM 53 00 53. REMOVED BRACKET REF B737 700 SRM 51 40 02. HEAT TREATED TO T6 CONDITION LOAD #HT112911 1 REF BAC DWG 149A8118 REV A. FABRICATED BRACKET REF BAC DWG 149A8118 REV A. ALODINED AND PRIMED BRACKET REF B737 700 SRM 51 20 01. PAINTED BRACKET REF B737NG AMM 51 21 99. INSTALLED BRACKET REF B737 700 SRM 51 40 02. BLEND OUT DIMENSION IS 44 IN LOG BY 2IN WIDE.

Part: SUPPORT — WORN (NR 1 PLYON) · airframe 41,172 hrs · 18,329 cycles

NR 1 PYLON PNL 431 AT AFT SUPPORT CENTER LOWER AREA WORN. REPAIRED FORWARD FRAME SUPPORT IAW REO 6 14308 REV A DATED 11 29 2011 AND EA 700 54EA 06958 DATED 30 NOV 2011.

Part: SUPPORT — WORN (NR 2 PYLON) · airframe 41,172 hrs · 18,329 cycles

NR 2 PYLON L/E FWD FAIRING SUPPORT CENTER LOWER SKIN WORN. REPAIRED FORWARD FAIRING SUPPORT IAW REO G 14307 REV A DATED 11 29 2011 AND EA 700 54EA 06958 DATED 30 NOV 2011.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,172 hrs · 18,329 cycles

AFT CARGO COMPARTMENT FLOOR STRINGER CORRODED AROUND TIE DOWN BS 747 RBL 14. REPAIRED IAW B737 700 SRM 53 00 53.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,172 hrs · 18,329 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SPLICES CORRODED BS 887 LBL 14 RBL 14. REMOVED PNL SPLICE AND FOUND TO BE OUT OF LIMITS AFTER CLEAN UP. REPLACED SPLICE.

Part: PLATE — WORN (FUSELAGE) · airframe 41,172 hrs · 18,329 cycles

ECS HIGH PRESSURE DOOR 192DR CUTOUT O/B LATCH STRIKE PLATE WORN. REPAIRED IAW EA 700 53EA 06961 AND REO 614310 REV B.

Part: SUPPORT ANGLE — CHAFED (FUSELAGE) · airframe 41,172 hrs · 18,329 cycles

ECS HIGH PRESSURE DOOR 192DR CUTOUT O/B EDGE SUPPORT ANGLE CHAFED ON EDGE. REPAIRED IAW EA 700 53EA 06961 AND REO 614310 REV B.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,420 hrs · 16,151 cycles

BATTERY PACK M1675 FAILED TIME LIMIT TEST REMOVED AND REPLACED BATTERY PACK.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 36,420 hrs · 16,151 cycles

FWD ENTRY DOOR INNER SKIN IS CRACKED AT AFT EDGE 3RD FROM BOTTOM STOP PIN FITTING CUTOUT. REMOVED DAMAGE FABRICATED REPAIR DOUBLER AND INSTALLED IAW EA 70 52 EA 03412.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

LOWER FLANGE ON FLOORBEAM CRACKED IN RADIUS. REMOVED AND REPLACED THE BS 269 FLOORBEAM UPPER CHORD.

Part: SUPPORT — CRACKED (CARGO BAY) · airframe 36,420 hrs · 16,151 cycles

AFT CARGO BAY VACUUM WASTE COMPARTMENT VERTICAL SUPPORT POST LOWER ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET WITH FABRICATED PART.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,420 hrs · 16,151 cycles

RT HORIZONTAL STAB LOWER SKIN STAB STA 120 18 INCHES FROM FRONT SPAR. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 36,420 hrs · 16,151 cycles

LEFT WING FIXED T/E CRACKED AT WING T/E FIXED BULKHEAD AT STA 289 SEAL SUPPORT FITTING. REPLACED BULKHEAD SEAL SUPPORT FITTING.

Part: DOUBLER — CRACKED (ECS EXHAUST) · airframe 36,420 hrs · 16,151 cycles

RIGHT ECS DUCT EXHAUST DUCT DOUBLER CRACKED. FABRICATED REPLACEMENT DOUBLER ASSY FOR THE RT ECS DUCT EXHAUST SLEEVE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

FWD CARGO PIT BAFFLE CLIP CRACKED. REMOVED AND REPLACED CRACKED CLIP.

Part: SUPPORT BRACKET — CRACKED (L2 DOOR) · airframe 36,420 hrs · 16,151 cycles

L2 DOOR AFT SUPPORT BRACKET CRACKED ON LOWER LINER SUPPORT. REMOVED AND REPLACED BRACKET.

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 36,420 hrs · 16,151 cycles

AFT CARGO BAY LINER LOWER SUPPORT BRACKET CRACKED. REMOVED DAMAGED PART, FABBED AND INSTALLED PART.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

INTERCOSTAL CRACKED AT BS 380 - 400. REMOVED CRACKED INTERCOSTAL AT BS 380 - 400 AND REPLACED WITH NEW INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

INTERCOSTAL IS CRACKED ON THE UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

FRAME IS CRACKED AT AC BRACKET ATTACH FASTENER HOLE. REPAIRED CRACKED FRAME AT BS 867.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

FRAME IS CRACKED AT STR 8 AC DUCT ATTACH BRACKET RIVET HOLE. FRAME WAS REPAIRED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

INTERCOSTAL IS CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

INTERCOSTAL IS CRACKED ON UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

INTERCOSTAL HAS TWO CRACKS ON THE UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

FRAME CRACKED AT AC ATTACH BRACKET FASTENER HOLE. REPAIRED CRACKED FRAME AT BS 400 STR 8 LT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

FRAME IS CRACKED AT AC BRACKET ATTACH FASTENER HOLE. REPAIRED BS 727D STR 8 LT FRAME AT A/C ATTACH BRACKET.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,420 hrs · 16,151 cycles

INTERCOSTAL IS CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 31,950 hrs · 13,971 cycles

LEFT AND RIGHT PANEL CHANNELS CRACKED AT STA 538 BL 0. REPAIRED CHANNELS IAW AAR EA 12908 AND ALASKA EA 5320 01851.

Part: SKIN — DENTED (CARGO DOOR) · airframe 31,949 hrs · 13,971 cycles

FWD CARGO DOOR HAS FIVE EA DENTS WITH CREASES BETWEEN STA 455 489 AND BETWEEN BEAMS NR 2 AND NR 4. REMOVED DAMAGED AREAS, FABBED DOUBLER AND INSTALLED THE REPAIR IAW EA 12906.

Part: SKIN — CHAFED (L/E SLAT) · airframe 31,949 hrs · 13,971 cycles

NR 5 SLAT LOWER SURFACE IS CHAFED AT INBOARD UPPER CORNER. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10.

Part: SKIN — CHAFED (L/E SLAT) · airframe 31,949 hrs · 13,971 cycles

NR 8 SLAT OUTBOARD END LOWER SURFACE IS CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10.

Part: SKIN — CHAFED (L/E SLAT) · airframe 31,949 hrs · 13,971 cycles

NR 4 SLAT LOWER T/E SURFACE IS CHAFED AT THE ENDS AND TRACK LOCATIONS ABOVE THE ACTR. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (NR 8 SLAT) · airframe 31,949 hrs · 13,971 cycles

NR 8 SLAT LOWER SURFACE T/E IS CHAFED AT THE ACTR. REMOVED DAMAGE, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10.

Part: SKIN — CHAFED (L/E SLAT) · airframe 31,949 hrs · 13,971 cycles

NR 7 SLAT INBOARD CORNER LOWER SURFACE CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10.

Part: FLOORBOARD — DAMAGED (LAVATORY) · airframe 27,145 hrs · 11,554 cycles

FWD LAV FLOOR BOARD DAMAGED AND DISBONDED REPAIRED IAW AMM 25 00 00.

Part: FLOORBOARD — CRACKED (BS 328-380) · airframe 27,145 hrs · 11,554 cycles

FLOORBOARD 222CF IS CRACKED AT CORNER AND EDGE REPAIRED IAW 53-00-50.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 27,145 hrs · 11,554 cycles

AFT CARGO COMPARTMENT DOOR HAD TWO CREASES IN IT REPAIRED IAW 52 30 01360.

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2

INTERCOSTAL AT STA 947 967 IS CORRODED REPAIRED IAW SRM 51 40 02.

Part: FLAP TRACK — WORN (TE FLAPS) · airframe 27,145 hrs · 11,554 cycles

LT INBD AFT FLAP OTBD TRACK HAS WORN PLATING REPLACED IAW AMM 27 51 16.

Part: FLOORBOARD — PUNCTURED (BS 294-344) · airframe 27,145 hrs · 11,554 cycles

CABIN FLOOR BOARD IS PUNCTURED ON UPPER SURFACE REPAIRED IAW SRM 53 00 50.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 27,145 hrs · 11,554 cycles

FLOORBEAM AT STA 950 IS CORRODED REPAIRED IAW 51 40 02.

Part: SUPPORT — CORRODED (BS 990-1016) · corrosion level 2 · airframe 27,145 hrs · 11,554 cycles

EXTRUSION AT STA 990 IS CORRODED AT FASTENER HOLES REPAIRED IAW SRM 51 40 02.

Part: FLAP TRACK — WORN (TE FLAPS) · airframe 27,145 hrs · 11,554 cycles

RT INBD AFT FLAP TRACK HAS WORN PLATING REPLACED IAW AMM 27 51 16.

Part: FLAP TRACK — WORN (TE FLAPS) · airframe 27,145 hrs · 11,554 cycles

RT INBD AFT FLAP OTBD TRACK HAS AREA OF WORN PLATING REPLACED FLAP TRACK IAW AMM 27 51 16.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,145 hrs · 11,554 cycles

FLOORBEAM AT STA 986.5 IS CORRODED AT FASTENER HOLES REPAIRED IAW EA 5310 02717.

Part: SILL — CORRODED (BS 277-294) · corrosion level 2 · airframe 27,145 hrs · 11,554 cycles

RI DOOR SILL STRAP IS CORRODED REPAIRED IAW SRM 51 40 2.

Part: INTERCOSTAL — CRACKED (BS 277-294) · airframe 27,145 hrs · 11,554 cycles

INTERCOSTAL CRACKED AT STA 277 REPAIRED IAW SRM 51 70 11.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,145 hrs · 11,554 cycles

FWD CARGO DOOR LOWER SILL WEB IS CORRODED REPAIRED IAW SRM 51-40-02.

Part: FLOORBOARD — CRACKED (BS 950-986) · airframe 27,145 hrs · 11,554 cycles

FLOORBOARD AT STA 950 IS CRACKED IN 8 LOCATION REPAIRED IAW SRM 53 00 50.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

AFT CARGO DOOR LOWER SILL WEB IS CORRODED REPAIRED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 950) · corrosion level 2 · airframe 27,145 hrs · 11,554 cycles

FLOOR SUPPORT AT STA 950 IS CORRODED ON UPPER FLANGE REPAIRED IAW SRM 51 40 02.

Part: FITTING — GOUGED (SPOILER ACTUATOR) · airframe 27,145 hrs · 11,554 cycles

NR 12 SPOILER LOCK GOUGED INTO SPOILER ACTUATOR FITTING. REPLACED IAW AMM 27 62 91.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,145 hrs · 11,554 cycles

AFT PIT FLOOR SUPPORT CORRODED AT STA 772 REPAIRED IAW EA5320 01799.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,145 hrs · 11,554 cycles

FLOORBEAM AT STA 344 UPPER FLANGE CORRODED REPAIRED IAW 5310 02716.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,145 hrs · 11,554 cycles

AFT PIT FLOOR SUPPORT CORRODED AT STA 772 REPAIRED IAW EA 5320 01799.

Part: SUPPORT — GOUGED (FUSELAGE) · airframe 27,145 hrs · 11,554 cycles

FWD PIT CARGO TIE DOWN IS GOUGED AT STA 495 REPAIRED IAW EA 5320 01821.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,118 hrs · 10,229 cycles

INTERIOR EMERGENCY EXIT LIGHTS OVER DOOR R2 INOP. SECURED LOOSE SOCKET, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND R2 DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED PACK POWER SUPPLY

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

DURING C-CHECK FOUND AFT CARGO PIT NR 2 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K)

Part: PLATE — CORRODED (FS 267)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR PANEL SPLICE PLATE. REPAIRED IAW SRM 51-40-02 AND 53-00-53. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

DURING C-CHECK FOUND AFT CARGO PIT NR 3 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FS 758-887)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 758. REPAIRED IAW SRM 53-00-53. (M)

Part: STOP FITTING — CHAFED (FS 344)

PAE - DURING C-CHECK, FOUND FORWARD ENTRY DOOR AFT LOWER STOP PIN FITTING IS CHAFED. REPLACED DOOR IAW MM 25-10-00. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K)

Part: SUPPORT — CORRODED (FS 500C)

PAE - DURING C-CHECK, FOUND FORWARD CARGO BAY FLOOR TO SIDEALL SUPPORT CORRODED. REPAIRED IAW SRM 51-40-02 AND 53-00-53. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 773. REPAIRED IAW EA. (K)

Part: SUPPORT — CORRODED (BS 500B)

PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT IS CORRODED AT BS 500B. REPAIRED IAW SRM 51-40-02 AND 53-00-53. (M)

Part: FLOOR PANEL — DENTED (FUSELAGE)

DURING C-CHECK FOUND AFT CARGO PIT NR 1 FLOOR PANEL DENTED AND PUNCTURED. REPAIRED IAW SRM. (K)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

DURING C-CHECK, FOUND FWD CARGO PIT NR 2 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND BULKHEAD LWR CENTER SUPPORT ANGLE IS CORRODED AT BS 500D. REPAIRED IAW SRM. (K)

Part: PLATE — CORRODED (FUSELAGE)

DURING C-CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPAIRED IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE: DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT BS 336. REPAIRED IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING C-CHECK FOUND INTERCOSTAL CRACKED AT BS320. REPAIRED IAW SRM. (K)

Part: ANGLE — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND BULKHEAD LT LOWER L ANGLE CORRODED AT BS 500D. REPAIRED IAW SRM. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 500C. REPAIRED IAW SRM. (K)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 500A. REPAIRED IAW SRM. (K)

Part: WEB — CRACKED (FUSELAGE)

PAE: DURING C-CHECK, FOUND CLOSE OUT WEB CRACKED AT BS 492. REPAIRED IAW SRM. (K)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE: DURING C-CHECK FOUND CORROSION ON INTERCOSTAL AT STA 747-767. REPAIRED IAW SRM. (K)

Part: PLATE — CORRODED (FUSELAGE)

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

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

PAE: DURING C-CHECK, FOUND FWD CARGO NR 3 FLOOR PANEL PUNCTURED. REPAIRED IAW SRM. (K)

Part: POWER SUPPLY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. EMERGENCY LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. EMERGENCY LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: FUSE — BLOWN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT THE L1 DOOR, ADJACENT TO THE FORWARD FLIGHT ATTENDANT JUMPSEAT WAS FOUND TO BE INOPERATIVE. REPLACED FUSE AND THE LIGHT OPERATED NORMALLY. (M)

Part: FUSE — BLOWN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT THE L1 DOOR, ADJACENT TO THE FORWARD FLIGHT ATTENDANT JUMPSEAT WAS FOUND TO BE INOPERATIVE. REPLACED FUSE AND THE LIGHT OPERATED NORMALLY. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

PDX - DURING LINE MAINTENANCE, THE RIGHT NR 2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY. THE EMERGENCY LIGHTS THEN OPERATED NORMALLY. (M)