N73275

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 74,178 hrs · 26,586 cycles

RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. ATTEMPTED TO REMOVE COVER BUT 2 NUT PLATES WERE BROKEN IN THE BACK. COMPLETED UP TO STEP 5 OF THE RH AFT EMERGENCY WING LIGHT ASSEMBLY REF AMM 33-51-04-960-802. COMPLETED LIGHT ASSY INSTALL UP TO STEP G12 AMM 33-51-04-960-802. DURING OPS CK FOUND 3 OUTSIDE LIGHTS INOPERATIVE, DOOR 1L, RT AFT OVERWING EXIT & RT MID AFT WING SLIDE. REPLACED EMERGENCY LIGHT BATTERY PACK M1671, BOTH RH LIGHTS OPS NORMAL. IAW AMM 33-51-06 & WDM 33-51-11. RELAMPED EXTERIOR EMERGENCY LIGHT AT DOOR L1, NO GOOD. R & R BATTERY PACK AND POWER SUPPLY (M1675) IAW AMM 33-51-04, AMM 33-51-06. OPS CHECKED GOOD.

Part: SKIN — DEBONDED (ZONE 600 FLAP) · airframe 74,050 hrs · 26,531 cycles

RIGHT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN DEBONDED SIGNAL NOTED, AREA L=1X1.25 INCHES. CLEANED, PREPPED, REPAIRED & RESTORED PAINT AT RT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN IAW SRM 57-5 3-01-2R-16, SRM 51-70-10-2R-0, AMM 51-21-41-370-803, AMM 51-21-72 -370-804, AMM 51-21-99-300-802, AND AMM 51-21-99-300-801.

Part: SKIN — CRACKED (ZONE 300) · airframe 74,058 hrs · 26,533 cycles

LH HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED L=1INCH APROX. AT STAB STA147.90 AND 15.600 INCH FROM FWD SPAR (REF AAR NR 1000060354) PERFORMED PERMANENT REPAIR AT LT HORIZONTAL STAB AT STAB STA147.90 AND 15.600 INCH FROM FWD SPAR THIS REPAIR IS A CATEGORY "B", REQUIRE REPETITIVE INSPECTIONS IAW B737 SRM 55-10-01-2R-11 STEP 5 A. INSPECTION REQUIREMENTS TABLE 204.

Part: SKIN — DEFORMED (ZONE 800) · airframe 74,050 hrs · 26,531 cycles

RE-SKIN AFT CARGO DOOR. REMOVED AND REPLACED AFT CARGO DOOR SKIN, ALL WORK PERFORMED IAW SRM 52-30-01-2R-3.

Part: SKIN — CRACKED (ZONE 300) · airframe 74,058 hrs · 26,533 cycles

RH HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED L=0.855INCH APROX. AT STAB STA157.10 AND 9 INCH FROM AFT SPAR (REF AAR NR 1000060368)PERFORMED PERMANENT REPAIR AT RH HORIZONTAL STAB AT STAB STA157.10 AND 9 INCH FROM AFT SPARTHIS REPAIR IS A CATEGORY "B", REQUIRE REPETITIVE INSPECTIONS IAW B737 SRM 55-10-01-2R-11 STEP 5 A. INSPECTION REQUIREMENTS TABLE 204.

Part: SKIN — NOT REPORTED (ZONE 800) · airframe 74,050 hrs · 26,531 cycles

RE-SKIN FWD CARGO DOOR. REMOVED AND REPLACED FWD CARGO DOOR SKIN, ALL WORK PERFORMED IAW SRM 52-30-01-2R-3

Part: CARGO NET — TORN (ZONE 100) · airframe 73,833 hrs · 26,417 cycles

FORWARD CARGO COMPARTMENT BIN THREE CARGO NET TORN. REFERENCE AIRCRAFT MAINTENANCE MANUAL FOUND CARGO NET TO BE SERVICEABLE. REPAIR OR REPLACE CARGO NET WITHIN 10 DAYS IN REFERENCE WITH AMM 25-52-04-200-801C1.

Part: TOILET — LEAKING (ZONE 900) · airframe 73,085 hrs · 26,071 cycles

LAV D FLUSHES CONTINUE OUSLY REF FIM 38-30 TASK 816 VERIFIED NO CLOG VERIFIED RINSE VALVE OPENS AND CLOSES SUSPECT FLUSH CONTROL ASSEMBLY NEEDS TO BE CHANGED REQUEST MEL 3802D REQUESTING MEL TOILET VALVE MANUALLY CLOSED IN ACCORDANCE WITH MEL. SLAVE IN LAV FLUSH SWITCH, NO HELP. REINSTALLED ORIG FLUSH SWITCH. R/R VACUUM TOILET ASSY PER AMM 38-32-01-000/400-838-002. OPS TESTS FOUND WATER CONTINOUSLY DRIPPING INSIDE THE BOWL AND COLLECTED IN THE LOWER PORTION. PART IS BAD OUT OF STOCK. MEL STAYS, PROCEDURES COMPLIED WITH. LAV D STILL INOP. REPLACED LAV D VACUUM TOILET ASSEMBLY REF AMM 38-32-01, OPS CHECKED GOOD.

Part: SWITCH — FAULTED (CARGO DOOR) · airframe 72,341 hrs · 25,712 cycles

FWD CARGO DOOR LIGHT WILL NOT EXTINGUISH WHEN DOOR IS CLOSED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN, PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V950348 MAC RELATED WORK ORDER 000000003132931 AND PRTR DOOR CONFIRMED SECURED CLOSED - PLACING ON DEFERRAL IN REF WIT MEL 5203D. PARANHOS, HAMSA (V950348) DOOR CONFIRMED SECURED CLOSED - PLACING ON DEFERRAL IN REF WIT MEL 5203D. DEFERRED DIRECTLY BY TOMC DISCONNECTED FWD CARGO DOOR SWITCH S960 GROUND WIRE AND STOWED. REPLACED FORWARD CARGO DOOR INDICATION SWITCH REF AMM 52-71-31. DOOR INDICATES PROPERLY. OPS CHECK GOOD AT THIS TIME.

Part: STRIP — MISSING (ZONE 300) · airframe 70,926 hrs · 25,048 cycles

OUTBOARD END OF R ELEVATOR APPEARS TO HAVE SHEET METAL DAMAGE A ND SEPARATION PHOTO UPDATE. DAMAGE IS TO THE RH HORIZONTAL STAB T/E PANEL CONDUCTIVE STRIP. THE DAMAGE EXCEEDS THE ALLOWABLE LIMITS IN SRM 55-10-01 ALLOWABLE DAMGE 3 AND FIG 9. PARTS USED: 99-2361-3-0101,QTY :1 29-5510-3-0115,QTY :1 REMOVED REMAINING CONDUCTIVE STRIP. LOCATED AND DRILLED NEW CONDUCTIVE STRIP REF AMM 55-10-01-300-801 AND SRM 55-10-01-2R-10 REPAIR 10. PARAGRAPH 5. L/P 9407581 CAN BE WORKED AT THE SAME TIME. PARTS USED: 00-0583-3-6863,QTY :1 29-5510-3-0126,QTY BONDED NEW CONDUCTIVE STRIP TO TRAILING EDGE WITH BMS5-95 B2 PER SRM 55-10-01-2R-10. INSTALLED BLIND RIVETS IN OUTER AND INNER ROWS PER IPC 55-10-00-08 AND SRM 51-40-03-0G-0 FOR FASTENER SUBSTITUTION. RIVETS ON TRAILING EDGE STILL NEED TO BE ADD EMP:U231979 :1 78-2361-3-0001,QTY :1 INSTALLED. WILL NEED BONDING CHECK AND PAINT WHEN SEALANT IS CURED. INSTALLED TRAILING EDGE FASTENERS ON CONDUCTIVE STRIP, PERFORMED RESISTANCE TEST AND PAINTED. REF SRM 55-10-01-2R-10

Part: STRINGER — CRACKED (LT WING) · airframe 69,983 hrs · 24,606 cycles

L/H WING BETWEEN RIBS 19 AND 20 UPPER STRINGER # 8 CRACKED AT TIP. SUPPORT TASK NSA EMX N/R 00222 ADDED SDR BLOCK CUT OUT DAMAGED SECTION OF U8 STRINGER AND REPAIRED.

Part: ANGLE — CRACKED (L/H PACK BAY) · airframe 69,983 hrs · 24,606 cycles

L/H PACK BAY AFT WALL REAR SPAR UPPER ANGLE CRACKED. SUPPORT TASK NSA EMX N/R00196.

Part: ANGLE — CRACKED (R/H PACK BAY) · airframe 69,983 hrs · 24,606 cycles

R/H PACK BAY AFT WALL REAR SPAR UPPER ANGLE CRACKED.SUPPORT TASK NSA EMX N/R00197.

Part: FITTING — CRACKED (BS 540 LBL32) · airframe 69,983 hrs · 24,606 cycles

B737-57-4-1262 SHEAR FITTING AT STA. 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00201.

Part: LIGHT — NO TEST (SEAT ROW 20ABC) · airframe 69,359 hrs · 24,338 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - AFT SEAT MOUNTED EMERGENCY LIGHT AT ROW 20ABC DAMAGED. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT REF MM 33-51-11. OPS CK OK. PARTS USED: BR9644-12,QTY :1 VERIFIED IDT REQUIREMENTS

Part: ENGINE — FAULTED (ENGINE #2) · airframe 67,135 hrs · 23,312 cycles

ENGINE 2 SHOWED 0 QTY DURING DESCENT ALONG WITH FLUCT PRESS. ENG PARAMETRS NRML. ADDITONAL CREW DEBRIEF: CREW DID NOT SHUT DOWN ENGINE, OIL PRESS URE REMAINED POSITIVE BUT DID FLUCTUATE FROM AMBER TO RED. ALL E NGINE PARAMETERS REMAINED NORMAL. PHOTOS OF LEAKING AREA FROM UNDER ENGINE AFTER PART BAG AND HIGH INFORMATION UPDATE, SDR FLAGGED POWER RUNS. REMOVED & REPLACED ENGINE #2 AS PER JOB CARD PER JOB CARD 58-7200-9-0001. OPS GOOD.

Part: FORGING — NONE (LH#1WINDOW) · airframe 66,491 hrs · 23,029 cycles

FOR ESFR REPORTING ONLY. EA 5310-04554 REV B OP005 ACCOMPLISHED FOR LH #1 WINDOW FRAME. EA 5310-04554 REV B OP005 REPAIR ACCOMPLISHED FOR CONFIG B.

Part: SENSOR — FAULTED (FUSELAGE) · airframe 66,164 hrs · 22,878 cycles

AUTO SLAT FAIL LT ILLUM DURING RECALL. EXTINGUISHES WHEN MC LIGH T PRESSED FSEU BITE SHOWS NO FAULTS, #2 SYMD SHOWS NO FAULTS, #1 SYMD FIM 27-32-809. PLACE #1 AUTOSLAT SYSTEM INOP PER MEL 2712A, DDP PLACED ON MEL 2712A, DDP C/W. SHOWS FAULT MSG 27-31004 AOA SENSOR SIGNAL ERROR. NEEDS T/S PER C/W. TOMC APPROVED MEL 2712A 34-21-05-730-801. A/S FAIL LIGHT DOESNT ILLUMINATE ON AMM 27-83-00-710-801. PARTS USED: RECALL.. STILL REQUIRES AUTOSLAT FUNCTIONAL TEST REF 29-3412-9-0001. RPLCD LEFT AOA SENSOR.REF AMM 34-21-05-000-801(400-801) .RMVD COLLAR AND CLOSED A/S DC1 C/B.SYSTEM TESTS GOOD ,REF TASK PERFORMED AUTO SLAT SYSTEM FUNTIONAL TEST AS PER AMM TASK AT THIS TIME. ALL CHECKS NORMAL. 27-83-00-710-801. FUNCTIONAL TEST PASSED NO DEFECTS OR FAULTS (AUTO SLAT FAIL) NOTED AT THIS TIME. PERFORMED OPS CHECK IF AOA (LEFT) AS PER AMM 34-21-05. SYSTEM TEST PASSED. NO DEFECTS NOTED

Part: SENSOR — DEFECTIVE (AOA LEFT) · airframe 66,164 hrs · 22,878 cycles

LOST CAPT VERTICAL F/D SPD LIM INDICATED ON PFD ALL SPD INDS AGG REED THEN LEFT STICKSHAKER LOG UPDATED AS INFO CONTAINED ON TOCS: BITE PERFORMED, SMYD PERFORMED LEFT AND RIGHT ADIRS BITE TEST, NO FAULTS FOUND. ...BITE ALSO SHOWED MULTIPLE ALTITUDE DISAGREE FAULTS. (REF LP 3566515 FOR AOA SENSOR R/R. )ALSO PERFORMED BITE OF BOTH FAULT 27-31004 L AOA SENSOR. PERFORMED DEU 1&2 BITE TEST, FOUND MULTIPLE AIRSPEED DISAGREE SYMD''S NO EXISTING FAULTS PRESENT. ALSO CK''D BOTH DEU''S ,ALSO NO FAULTS ON THE LAST 7 LEGS DEU 1&2. MAINT MESSAGES 31-65050 & CURRENT FAULTS NOTED. 31-65060. NEEDS FURTHER T/S. REF LP 3566515, (R/R OF LEFT AOA SENSOR) PERFORMED OPS CHECK OF AMM 27-83-00. OPS CHECK/FUNCTIONAL CHECK GOOD. NO DEFECTS OR LEFT AOA SENSOR AS PER AMM 34-21-05. NO DEFECTS OR FAULTS NOTED FAULTS NOTED AT THIS TIME. AT THIS TIME. ALL ADIRU AND SMYD CHECKS OK AND NO CURRENT FAULTS. PERFORMED FUNCTION CHECK ON LE AUTOSLAT SYSTEM AS PER

Part: FLANGE — CRACKED (HORIZONTAL STAB) · airframe 65,918 hrs · 22,756 cycles

LT HORIZ STAB INTERNAL HORIZ FLANGE IS CRACKED STA 92.70 .5" AFT OF STIFFENER #1 TO LWR SKIN ATTACHMENT. REPAIRED LH HORIZ STAB LOWER CHORD AT STA 92.70 AT STIFFENE #1 I AW SRM 55-10-09-2R5 REPAIR 5 FIG 202 AND 203. DATA WAS TRANSCRIB ED FROM PAPER DOC AERSALE WO 3713 OP 24081. BY MECH V928682 INSP AQC023.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 65,918 hrs · 22,756 cycles

DURING C-SCAN INSPECTION AT GYR DURING D-CHECK, A CRACK WAS FOUND ON THE RH HORIZONTAL STABILIZER AT STA 157.10 23" FROM FORWARD SPAR, 17" FROM AFT SPAR. CRACK MEASURED .5". WORK TRANSCRIBED FROM AERSALE NON-ROUTINE 23985. 23 WITH NO DEFECTS NOTED. DOUBLER MANUFACTURED AND INSTALLED PER L WORK TRANSCRIBED ON AERSALE NON-ROUTINE 23985. INSPECTION THRE ERY 9000 FLIGHT CYCLES THEREAFTER REPAIR 11, DOUBLER THICKNESS 0.090" AND MEASURED 10" X 10". AL SHOLD 56000 TOTAL FLIGHT CYCLES AND THEN PERFORM DVI AND LFEC EV REPAIRED CRACK DAMAGE PER SRM 55-10-01-2R REPAIR 11 PARAGRAPH 4B .2 FIG 204. HFEC PERFORMED PER NDT MANUAL 6-51-00-00 PROCEDURE

Part: FLAP — NONE (PRIMARY) · airframe 63,975 hrs · 21,939 cycles

*EMERGENCY DECLARED* PRIMARY FLAPS FAILED AT FLAP 1. EXTENDED FLAPS WITH ALTERNATE FLAP SYSTEM INSPECTED PER AMM 27-51-00-210-801. NO DAMAGE NOTED. PERFORMED FSEU BITE REF FIM 27-51 TASK 801. MSG 27-52259. PERFORMED FAULT ISOATION PER FIM 27-51 TASK 813. NO CURRENT FAULTS. PERFORMED OPERATIONAL TEST OF FLAP SYSTEM REF MM 27-51-00. OP CHECK GOOD. ADD EMP:U332421

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 61,958 hrs · 21,107 cycles

EMERGENCY LIGHT ON SEAT ROW 36 ABC LENS DAMAGED. REMOVED AND REPLACED WHITE EMERGENCY LIGHT REF MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS

Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 60,392 hrs · 20,527 cycles

EGT, FF, OIL PRESSURE, AND OIL TEMPERATURE INDICATIONS CONTINUE TO SHOW AFTER ENGINE SHUTDOWN LEFT ENGINE ON MAX THRUST BLDS OFF T/O...EGT ENG 1 EXCEEDED LIMIT TO 988 AT ROTATION UNTIL THRUST REDUCTION CREW REPORTED EXTREMELY HOT DAY, EGT SLOWLY CLIMBED DURING TAKE-OFF AND EGT INDICATION TURNED RED ALL OTHER ENG PARAMETERS NORMAL. SEE PHOTO OF THE ENG EXCEEDANCES PAGE. ACPD EEC BITE, NO EGT FAULTS #1 ENG. INPUT MONITORING ALL WITHIN LIMITS PER FIM77-21-00-810-803-FOO PARA E(1)F PG3. INSPECTION OF INLET AND EXHAUST AREAS OF THE ENG NO DESCRIPENCIES FOUND. OPEN ENG FOR BOROSCOPE INSPECTION OF HPT BLADES REF TASK72-00-00-200-807-F00 AND STAGE 1 LPT BLADES REF REF TASK 71-06-00-810-805-F00 AND TASK 71-00-00-800-804-F00 ACP TASK72-00-00-200-808-F00. ACP''D ENGINE #1 HPT BLADES BORO INSPECTION REF TASK NOTED. BLADES OKAY FOR CONTINUED SERVICE. INSPECTION REF TASK 72-00-00-200-808-F00. NO LIMITING DEFECTS 72-00-00-200-807-F00 AND ENGINE #1 STAGE 1 - 3 LPT BLADES BORO REFERENCED MM. INSTALLED BORO PLUGS AND GEARBOX DRIVEPAD COVER AS PER QC VERIFIED INSTALL OF BORO PLUGS AND CRANK PAD COVER ON #1 ENG. PER IDT LIST GMM 09-10-05. AND RII LIST GMM 09-25-05. IGNITION SYSTEM AUDIBLE TEST AS PER TASK 74-00-00-750-801-F00. ALL CHKS GOOD. DUE TO IGNITER PLUG REMOVAL FOR BOROSCOPE INSPECTION ACP''P PER FIM TASK 71-06-00-801-805-F00 COMPLETED ITEM F. (3)(A) TEST 1 PNEUMATIC LEAK CHECK AS PER TASK 71-00-00-700-809-F00. NO LEAKS FOUND ON THE ENG OR UPSTREAM OF THE PRSOV. ACP''D ENG BLD A

Part: ENGINE — UNKNOWN · airframe 60,392 hrs · 20,527 cycles

EGT, FF, OIL PRESSURE, AND OIL TEMPERATURE INDICATIONS CONTINUE TO SHOW AFTER ENGINE SHUTDOWN LEFT ENGINE ON MAX THRUST BLDS OFF T/O...EGT ENG 1 EXCEEDED LIMIT TO 988 AT ROTATION UNTIL THRUST REDUCTION CREW REPORTED EXTREMELY HOT DAY IN DEN, EGT SLOWLY CLIMBED DURING TAKE-OFF AND EGT INDICATION TURNED RED ALL OTHER ENG PARAMETERS NORMAL. SEE PHOTO OF THE ENG EXCEEDANCES PAGE. ACPD EEC BITE, NO EGT FAULTS #1 ENG. INPUT MONITORING ALL WITHIN LIMITS PER FIM77-21-00-810-803-FOO PARA E(1)F PG3. INSPECTION OF INLET AND EXHAUST AREAS OF THE ENG NO DESCRIPENCIES FOUND. OPEN ENG FOR BOROSCOPE INSPECTION OF HPT BLADES REF TASK72-00-00-200-807-F00 AND STAGE 1 LPT BLADES REF REF TASK 71-06-00-810-805-F00 AND TASK 71-00-00-800-804-F00 ACP TASK72-00-00-200-808-F00. ACP''D ENGINE #1 HPT BLADES BORO INSPECTION REF TASK NOTED. BLADES OKAY FOR CONTINUED SERVICE. INSPECTION REF TASK 72-00-00-200-808-F00. NO LIMITING DEFECTS 72-00-00-200-807-F00 AND ENGINE #1 STAGE 1 - 3 LPT BLADES BORO REFERENCED MM. INSTALLED BORO PLUGS AND GEARBOX DRIVEPAD COVER AS PER QC VERIFIED INSTALL OF BORO PLUGS AND CRANK PAD COVER ON #1 ENG. PER IDT LIST GMM 09-10-05. AND RII LIST GMM 09-25-05. IGNITION SYSTEM AUDIBLE TEST AS PER TASK 74-00-00-750-801-F00. ALL CHKS GOOD. DUE TO IGNITER PLUG REMOVAL FOR BOROSCOPE INSPECTION ACP''P PER FIM TASK 71-06-00-801-805-F00 COMPLETED ITEM F. (3)(A) TEST 1 PNEUMATIC LEAK CHECK AS PER TASK 71-00-00-700-809-F00. NO LEAKS FOUND ON THE ENG OR UPSTREAM OF THE PRSOV. ACP''D ENG BLD A

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,056 hrs · 19,974 cycles

EA 5510-01843 REV H HORIZ STAB LOWER IN SPAR SKIN PANEL C-SCAN I NSP REVEALED 3 EA CRACKS LEFT HAND LOWER SURFACE 2 INBD SIDE OF STA 120.3, 9"-9.5" & 17"-18" AND 1 ON INBD SIDE OF STA 129.5 25" TO 26" ALL FWD OF REAR SPAR. REPAIRED 3 EA CRACKS ON HORIZ STAB LOWER SKIN REF SRM 55-10-01 R EPAIR 11 PG 201-224. DATA WAS TRANSCRIBED FROM PAPER DOC N/R 372 1990.

Part: PROXIMITY SENSOR — MALFUNCTIONED (LE FLAPS) · airframe 57,216 hrs · 19,264 cycles

LEADING EDGE SLATS TRANSIT LIGHT STAYS ON 1 LE TRANSIT LIGHT CYCLING ON/OFF WITH FLAPS UP #1 LE FLAP LIGHT ON OVHD & FWD LE FLAPS TRANSIT LIGHT ARE ON STEADY WITH FLAPS UP. FSEU BITE HAS MSG "F1 PROX RETRACT" 27-81216.F2 PROX RETRACT 27-81218 & F3 PROX RETRACT 27-81220.

Part: LATCH — DAMAGED (ACCESS DOOR) · airframe 56,176 hrs · 18,856 cycles

PTY OPERATIONS ADVISED PNEUMATIC ACCESS DOOR HAS ONE INOP LATCH PLEASE SPEED TAPE AS PER ECRA AS DISCUSSED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V912214 MAC RELATED WORK ORDER 000000001624161 AND PRTR TECH PERFORMED INTERIM REPAIR PER ECRA 5240-01384 TECH PERFORMED INTERIM REPAIR PER ECRA 5240-01384. CK TAPE PRIOR TO EACH DEPARTURE AND PERFORM PERMANENT REPAIR WITHIN 3 DAYS. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED. QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. R&R 1 LATCH AND 1 HINGE IAW ECRA 5240-01384 PART 3--PERMANENT RE PAIR. TOMCQC REV PERFORMED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,055 hrs · 16,852 cycles

EMERGENCY LIGHTS AT SEAT ROW 20ABC AND BETWEEN SEAT ROWS 28DEF AND 29DEF IN BULLNOSE INOP. RELAMPED EMERGENCY LIGHTS AT SEAT ROW 20ABC AND BETWEEN SEAT ROWS 28DEF REF 33-42-02-960-801. OPS CHECK NORMAL.

Part: ALTIMETER — UNSERVICEABLE (COCKPIT) · airframe 49,628 hrs · 16,314 cycles

AT FL310 CAPTAIN AND F/O ALTIMETER READ 3100, STANDBY ALTIMETER READS 30720. R&R STANDBY ALTIMETER PER AMM 34-13-01. A/C OK TO CONTINUE.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,378 hrs · 16,200 cycles

LEFT HORIZONTAL STAB SKIN CRACKED AT REAR SPAR BETWEEN HSS 92.7 AND 101.9. REPAIRED THE SKIN IAW SRM 55-10-01 REPAIR 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,378 hrs · 16,200 cycles

LT HORIZONTAL STAB LOWER SKIN CRACKED AT HSS 101.90 AND ABOUT 12 INCHES FWD OF EXISTING REPAIR. INSTALLED REPAIR DOUBLER IAW SRM 55-10 -01 REPAIR 11.

Part: BEAM — CRACKED (R1 DOOR) · airframe 49,378 hrs · 16,200 cycles

PERFORMED ALUMINUM SURFACE INSPECTION IAW SOPM 20-20-02 ON R1 DOOR FOUND LOWER BEAM IS CRACKED. REPAIRED. REMOVED AND REPLACED R1 DOOR LOWER BEAM IAW EC/ RA 5210-02750 AND SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,826 hrs · 14,928 cycles

AIRCRAFT DAMAGE, SCRATCH AT RT SIDE STATION 500 D. TOMC CHANGED BACK TO 0275. TOMC CORRECTED ACFT NR TO REFLECT 0411. REMOVED DAMAGED AREA & INSTALLED INTERIM REPAIR IAW ECRA 5331-02041. DIP INITIATED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 05 AUG 16. PLANNING TO CONTACT ENGINEERING AFTER 05 JUN 16, BUT BEFORE 05 JUL 16 FOR PERMANENT REPAIR.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 43,383 hrs · 14,066 cycles

LEFT AFT GALLEY EMER PATHWAY LIGHT INOPERATIVE, FOUND CONNECTOR D40044J DISCONNECTED. RECONNECTED CONNECTOR D40044J IAW SWPM 20-72-24 & AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,348 hrs · 14,055 cycles

FORWARD CABIN EMER LIGHTS INOPERATIVE. R & R PAX CABIN LIGHTING EMER CHARGER BATTERY PACK FWD IAW AMM 33-51-06. OPERATIONS CHECKED GOOD IAW AMM 33-51-0 6.

Part: FITTING — CRACKED (FUSELAGE) · airframe 43,348 hrs · 14,055 cycles

SUPPORT TASK CRACK FOUND IN SEAT TRACK BATHTUB FITTING AT RT STATION 727B RBL 24.75. R & R BATHTUB FITTING AT RT STATION 727B RBL 24.75 IAW EA 5320-02076 & SRM 51-40-02.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 33,284 hrs · 10,522 cycles

SUPPORT TASK - AFT PRESSURE BULKHEAD STA 1016 AFT SIDE AT APPROX STR 22R THERE IS A SHARP DENT FACING AFT (MARKED) AFT PRESS BLKD REPAIRED IAW ECRA 5310-05407. ACCOMP A PERMANENT REPAIR PRIOR TO 46,522 TOTAL FLT CYC'S. PLANNING TO CONTACT ENGINEERING AFTER 39,522 TOTAL FLT CYC'S BUT BEFORE 40,522 TOTAL FLT CYC'S FOR A PERMANENT REPAIR. ACCOMPLISH PERMANENT REPAIR PRIOR TO 46,522 TOTAL FLIGHT CYCLE PLANNING TO CONTACT ENGINEERING AFTER 39,522 TOTAL FLT CYCLES BUT BEFORE 40,522 TOTAL FLT CYCLES FOR PERMANENT REPAIR.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,284 hrs · 10,522 cycles

SUPPORT TASK - A/C BRACKET AT FRAME 440R INBOARD RIVET SHOW CRACK INDICATION (ALSO VISUALLY). REPAIRED AS PER EA 5310-04716 REV C OP 2.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,284 hrs · 10,522 cycles

A/C BRACKET AT FRAME 380R INBOARD RIVET SHOWS CRACK INDICATION. REPAIRED A/C BRACKET AT FRAME 380R, REF EA 5310-04716 REV C.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,284 hrs · 10,522 cycles

CRACKED INTERCOSTAL AT LBL 44 BETWEEN FUSELAGE STA 328 & 344. REMOVED AND REPLACED CRACK INTERCOSTAL AT INDICATED AREA PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,284 hrs · 10,522 cycles

CRACKED INTERCOSTAL AT FUSELAGE FLOOR STA 312 TO 328 AT RBL 30. REMOVED AND REPLACED CRACK INTERCOSTAL AT INDICATED AREA PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,284 hrs · 10,522 cycles

CRACKED INTERCOSTAL AT LBL 46 BETWEEN FUSELAGE STA 312 & 328. REMOVED AND REPLACED CRACK INTERCOSTAL AT INDICATED AREA PER SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,869 hrs · 9,677 cycles

L-1 FWD EMERGENCY LIGHTS OUT. R&R BATTERY PACK REF AMM 33-51-06, OPS CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,779 hrs · 8,536 cycles

EMERGENCY LIGHTS AT LEFT AFT OVERWING AND DIRECTLY AFT OF LEFT WING ARE INOPERATIVE. T/S PER WD 33-51-13 AND FOUND EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY PACK BAD, REPLACED BOTH. CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,076 hrs · 8,266 cycles

L1 AND L2 DOORS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FRONT LEFT AND AFT LEFT EMERGENCY LIGHT POWER SUPPLY BATTERY PACKS IAW AMM 33-51-06. OPS CHECKS GOOD.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 26,712 hrs · 8,137 cycles

RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN CRACK STATION SS 101.90 RUNNING FWD AND AFT "1" LENGTH C SCAN. (AFT I/B OF 3RD DRAIN HOLE) PER ECRA 5510-02042. NEED TO ACCOMPLISH AN INITIAL INSPECTION PRIOR TO 17,137 FLIGHT CYCLES AND THEN REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 9000 CYCLES PER PART 2 OF ECRA 5570-02042.