N73406

Part: SERVICE DOOR — MISSING (ZONE 100) · airframe 66,099 hrs · 27,682 cycles

LAV SERVICE PANEL MISSING UP[ON ARRIVAL REQUEST CDL 52D ADD PICS INSPECTED AREA NO DAMAGE NOTED AT THIS TIME. TECH CONFIRMED SIZE OF PANEL IS LESS THAN 150 SQINCHES.

Part: UNKNOWN — HAZE (ZONE 200) · airframe 65,583 hrs · 27,455 cycles

UPON LANDING PAX AROUND 24F SAW A MIST COMING OUT NEAR WINDOW AND A FUMES SMELL INSPECTED AREA NO SMELL OR MIST NOTED. OKAY TO CONTINUE

Part: BRAKE DISC — BROKEN (ZONE 700) · airframe 64,949 hrs · 27,165 cycles

FOUND #3 MLG BRAKE DAMAGED DURING TIRE CHANGE. SEE PHOTO. REMOVED AND REPLACED #3 BRAKE ASSY REF AMM 32-41-41. PARTS USED: 60-3241-9-0001,QTY :1 ROTABLE PARTS CHG:TT # 1381486 SN OFF 0407 PN OFF 60-3241-9-0001 IPC REFERENCE # NO COMPONENT FOUND.

Part: LIGHT — BROKEN (ZONE 200) · airframe 64,737 hrs · 27,064 cycles

SEAT 27C EMERG EXIT LIGHT BROKEN REPLACED EMERGENCY LIGHT ASSY REF AMM 33-51-11. LIGHT OPERATION NORMAL

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 64,692 hrs · 27,042 cycles

STATION 663 BULKHEAD VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROXIMATELY RBL 9.0

Part: FITTING — CRACKED (ZONE 200) · airframe 64,692 hrs · 27,042 cycles

SHEAR FITTING AT STA 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00091. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 DATA WAS TRANSCRIBED FROM NSA EMX N/R 00091 AND HANGER N/R IAW B737-900 SRM 51-40-02-0G AND BAC DRAWING 111A2000 REV 6481048. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 IAW B737-900 SRM 51-40-02-0G AND BAC DRAWING 111A2000 REV ORIGINAL FOR WORK ACCOMPLISHED SEE NSA EMX N/R 00091 AND HANGER N/R 6481048 SFR ID # 3860234 ATTACHED AND CIR C/W.

Part: FITTING — CRACKED (ZONE 200) · airframe 64,692 hrs · 27,042 cycles

SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00090. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 DATA WAS TRANSCRIBED FROM NSA EMX N/R 00090 AND HANGER N/R IAW B737-900 SRM 51-40-02-0G AND BAC DRAWING 111A2000 REV 6481047. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 IAW B737-900 SRM 51-40-02-0G AND BAC DRAWING 111A2000 REV ORIGINAL

Part: FITTING — CRACKED (ZONE 200) · airframe 64,692 hrs · 27,042 cycles

SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00092. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04. IAW B737-900 SRM 51-40-02-0G AND BAC DRAWING 111A2000 REV 6481049. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 IAW B737-900 SRM 51--40-- 02-0G AND BAC DRAWING 111A2000 REV ORIGINAL FOR WORK ACCOMPLISHED SEE NSA EMX N/R 000921 AND HANGER N/R 6481049 SFR ID # 3860296 ATTACHEDAND CIR C/W.

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 64,602 hrs · 27,002 cycles

RH AFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. REPLACED FUSE IN POWER SUPPLY M1671 REF WDM 33-51-13-5 AND AMM 33-51-06.

Part: FUSE — BLOWN (ZONE 200) · airframe 63,764 hrs · 26,634 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - RH AFT OVERWING ESCAPE LIGHT AND OVERWING ESCAPE GROUND ILLUMINATION LIGHT INOP RELAMPED BOTH LIGHTS REF AMM 33-51-04-960-801. STILL INOP. REPLACED BATTERY PACK REF WDM 33-51-13-5 AND AMM 33-51-06-960-805. NO FIX. SUSPECT BLOWN FUSE IN CHARGER. FOUND 1 BLOWN FUSE AND ANOTHER BARELY INSTALLED. REPLACED BOTH FUSES REF AMM 33-51-06-960-804.PARTS USED: 99-3351-3-0015,QTY :1 ABS-B215-06,QTY :2 767,QTY :2 OPC NORMAL REF AMM 33-51-00-710-801.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,891 hrs · 26,232 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M16171 FAILS OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,891 hrs · 26,232 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M1899FAILS OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,891 hrs · 26,232 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M1695 FAILS OPER ATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,891 hrs · 26,232 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M1694 FAILS OPERA TIONAL CHECK.

Part: SKIN — UNKNOWN (FWD CARGO DOOR) · airframe 62,891 hrs · 26,232 cycles

PER UAL REQUEST; REPLACE FWD CARGO DOOR SKIN. (REF: AAR NR 100011692) REMOVED AND REPLACED FWD CARGO DOOR SKIN IAW B737-90 SRM 52-30-0 1-2R-3.

Part: SKIN — UNKNOWN (AFT CARGO DOOR) · airframe 62,891 hrs · 26,232 cycles

PER UAL REQUEST; REPLACE AFT CARGO DOOR SKIN. (REF: AAR NR 100011693) REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW B737-900 SRM 52-30-01-2R-3 (REF: SFR#1036538)

Part: WINDOW FRAME — NONE (R1 WINDOW) · airframe 62,891 hrs · 26,232 cycles

CUST-REQ COMPLY WITH THE SSFR FORM FOR THE RH WINDOW MOD. (REF. AAR NR 100012042) COMPLIED WITH SSFR FOM AND LOG PAGE TO INFORMED EA5310-04554 REV C-OP-004 ON NO.1 RT SIDE WINDOW MOD COMPLETION. SSFR FOR ATTACHE D REFERENCE.

Part: PSEU — FAILED (FLIGHT COMPARTME) · airframe 57,479 hrs · 23,603 cycles

LEFT FWD OVERWING AND LEFT AFT OVERWING DOOR LIGHTS IN FLIGHT PERFORMED FIM TASK 52-20 TASK 801 FROM STEP A UP TO AND INCLUDING STEP E.(2) A. FAULTS ARE CLEARED, DOOR LIGHTS ARE OUT, WAS INTERMITTANT FAULT PER FIM. A/C RESTORED TO NORMAL (ALL CIRCUIT BREAKERS CLOSED). C/W FIM 52-20 TASK 801 OVERWING EXIT DOOR FLIGHT LOCK SWITCH FAULT ISOLATION.CODE 52-72007,52-72006 SEE LOG 8767656 REMOVED AND REPLACED PSEU

Part: NONE — FAILED (FLIGHT DECK) · airframe 57,250 hrs · 23,496 cycles

STANDBY IAS STANDBY IAS STUCK AT 159 KIAS. TAKEOFF REJECTED TO R EJECTED AT 110 LOCKING LOG DUE TO RTO UNLOCKED FOR SIGNOFF REMOVED AND REPLACED STANDY ALT./ AIRSPEED IND PER AMM 34-13-01. STANDBY IND. OPS NORMAL. ALSO PERFORMED LOW LEVEL PUMP UP PER AMM 31-11-00 FOR INDICATOR INDICATION. INDICATION NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1876103 SN OFF 0184 INSPECTED IDT ITEMS INDICATOR, AIRS OFF 29-3413-9-0002 0184 ON 29-3413-9-0002 0213

Part: FLAP — NONE (L.E) · airframe 57,233 hrs · 23,489 cycles

*EMERGENCY*LE FLAP TRANSIT CAUTION LIGHT LEFT OUTBOARD SLAT RAN FLAPS #1 SLAT NO AMBER LIGHT AND NO GREEN LIGHT AT 15. ACCOMPLISHED FIM 27-81 TASK 809 THRU STEP D NO ACTIVE FAULTS INDICATED. ACCOMPLISHED FIM 27-51 TASK 801 HAVE FAULT HISTORY FLIGHT LEG 1-- SL1 PROX INBOARD MSG 27-81201 LOCKED THE LOG ITEM DUE TO EMERGENCY DECLARED FOR LANDING. UNLOCKED TO WORK REPLACED 1 SLAT INBOARD SENSOR (S995) REF AMM 27-88-11-000-801,ACP OPS CHECKS,AMM 27-88-11-701-801 ,ALL CHKS AND FLT DECK INDICATIONS GOOD ADD EMP:U108812

Part: SKIN — NONE (STA 351) · airframe 56,437 hrs · 23,129 cycles

STA.351 STR. 2L DENT OUT OF LIMITS. (REF. F/C N/R 9796454) BEFORE 50,000 TOTAL AIRCRAFT FLIGHT CYCLES". REPAIRED PER ECRA 5330-06900 . ALL WORK PERFORMED ON F/C N/R 9796454. PLACED ON DIP TO "ACCOMPLISH A PERMANENT REPAIR ON OR

Part: PRESSURE WEB — CRACKED (STA663.75) · airframe 56,437 hrs · 23,129 cycles

FOUND 2EA CRACKS IN VERTICAL PRESSURE WEB AT STA 663.75 AND APPROX LBL 33. REF FLEET CYCLE N/R 9793198.CARD COMPLETE SEE WIPS AND TASKS FOR WORK PERFORMED.PER AMM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE DIP 57-DIP NO TASK AND LIMITATIONS ENTERED INTO CORRECTIVE ACTION. ALL INSPECTIONS COMPLETED REFERENCE FLEETCYCLE N/R 9793198. ADD EMP:U180693 U248732 U248935 REQUIREMENTS PER SRM 57-10-10-2R-3 ALT. 1 TABLE 204 PG 6. INSTALLATION. HFEC AND LFEC INSPECTIONS AT INTERVAL OF 36,000 INSPECTION THRESHOLD: 56,000 FLIGHT CYCLES AFTER REPAIR FLIGHT CYCLES. REPAIRED PER SRM 57-10-10-2R-3 ALT. 1. REF. F/C N/R 9793198 FOR ALL WORK PERFORMED. . PLACED ON DIP TO PERFORM INSPECTION APPROVED TO PERFORM AN INSPECTION HFEC AND LFEC WITH AN INITIAL TOMC-APPROVAL FROM SC1ELBYC COMMENT THRESHOLD OF OF 56,000 FLT CYCLES WITH REPEAT INSPECTIONS EVERY 36,000 FLY CYCLES IN REFERENCE WITH SRM 57-10-10-2R-3. TOMC APPROVED : QC REVIEWED. ACCOMPLISHED SFR #1027345 TOMC APPROVED : QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SKIN — CRACKED (STA101.90) · airframe 56,437 hrs · 23,129 cycles

REF FOR FLEET CYCLE...L/H HORIZONTAL STAB. LWR SKIN STA. 101.90 HAS CRACK INDICATION 14" AFT OF FRONT SPAR.(MARKED) ACCOMPLISHED SFR 1027346 -01-2R-11. 5A TABLE 204, "REPEAT INSPECTIONS 56,000 TOTAL FLIGHT FREQUENCY EDDY CURRENT INSP. PER 737 NDT PART6. 51-00-26, FIGURE CYCLES- DETAIED VISUAL INSP.9000 FLIGHT CYCLES &EXTERNAL LOW 1 REF FLEET CYCLE LP 9793313. REPAIREDL/H HORIZONTAL STAB. LOWER S KIN STA.101.90 IAW SRM 55-10-01-2R-11. INITIAT DIP PER SRM 55-10 ITEM NOT RII PER GMM-09-25-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,762 hrs · 22,347 cycles

AFT GALLEY DOOR AREA EMERGENCY LIGHTS ARE OUT. REPLACED EMER EXIT LIGHT BATTERY PACK AND OPS TEST GOOD. REF AMM 33-51-06-960-805. INSPECTED EMERGENCY LIGHT, OPS CHECK GOOD.

Part: THERMOCOUPLE — OUT OF LIMITS (RT ENGINE) · airframe 52,483 hrs · 21,320 cycles

RT ENG EGT LIM EXCEEDED ON CLIMBOUT ...SLIGHT THROTTL REDUC BROU GT TEMP INTO LIMS CJ HARNESS REPLACED, REF L/P 8182160. R+R S4 PROBE IAW AMM 77-21-01-400-801-FOO DUE TO DASHES ON EEC BITE. PERFORMED T49.5 PROBE AND EGT SYS INSP IAW AMM 77-21-01-200-801-F00, ALL VALUES WITHIN LIMITS. RAN ENG AT IDLE, ALL T49.5 PARAMETERS NORMAL. REF L/P 8183730 FOR POWER ASSURANCE CHECK. ADD EMP:U115824 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1647299 SN OFF 8456 IPC REFERENCE # PROBE, THERMOCO OFF 29-7721-9-9001 8156 ON 29-7721-9-9001 7072

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,892 hrs · 20,143 cycles

EXTERIOR EMERGENCY LIGHT AFT OF THE RT WING IS INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-04-960-801, OPS. CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,816 hrs · 20,110 cycles

RIGHT AFT OVERWING EXIT EXTERNAL EMERGENCY EXIT LIGHT AND THE RIGHT GROUND ILLUMINATION EMERGENCY LIGHT AFT OF THE WING ARE INOP. REMOVED AND REPLACED POWER SUPPLY FOR EMERGENCY EXIT LIGHTS AT APPROX STA 727. OPS CHECK GOOD. REF AMM 33-51-06-960-806.

Part: BATTERY — FAILED (ELT) · airframe 49,322 hrs · 19,888 cycles

AFT CABIN EMERGENCY LOCATOR TRANSMITTER DOES NOT TEST. REMOVED AND REPLACED THE AFT CABIN EMERGENCY LOCATOR TRANSMITTER BATTERY IAW AMM 25-64-00. BITE TESTED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,192 hrs · 19,821 cycles

AFT 7 ROWS OF THE EMERGENCY LIGHTS ARE INOPERATIVE, AND TWO AFT RT AISLE EMERGENCY LIGHTS ALSO INOPERATIVE. R & R THE BATTERY PACKS, OPS CHECKED GOOD IAW AMM 33-51-11.

Part: STRAP — INADEQUATE (L1 DOOR) · airframe 48,842 hrs · 19,666 cycles

L1 RED DOOR STRAP WONT FASTEN IN PLACE TO MARK ESCAPE SLIDE ARMED ADJUSTED SNAP, OPS CKS NORMAL.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 48,596 hrs · 19,556 cycles

DURING INSPECTION OF THE LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN PANEL, FOUND A CRACK AT HSS 175.5 ABOUT 25.5 INCHES FROM FORWARD L/E SPAR LOOKING AFT. INSTALLED CATEGORY B REPAIR DOUBLER IAW SRM 55-10-01, REPAIR 11.

Part: OVEN — FIRE (GALLEY) · airframe 48,161 hrs · 19,355 cycles

FRONT GALLEY OVEN FOOD CAUGHT FIRE. EXTINGUISHED WITH HALON EXTINGUISHER OVEN POS 205. R&R OVEN 205 FOR FOOD FIRE, OVEN OPS CK GOOD.

Part: BATTERY — DISCHARGED (ELT) · airframe 48,060 hrs · 19,309 cycles

AFT ELT DID NOT TEST. REMOVED AND REPLACED AFT ELT BATTERY IAW AMM 25-64-00-800-801C1, OPS CHECKED GOOD.

Part: BALLAST — FAULTY (CABIN) · airframe 48,054 hrs · 19,306 cycles

OVERWING EXIT LIGHT ABOVE EXIT SEAT 20F BURNT OUT. REMOVED AND REPLACED OVERWING EXIT BALLAST AND BULB. 20F SIDEWALL LIGHT OK FOR SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 47,692 hrs · 19,147 cycles

M1675 EMRGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,692 hrs · 19,147 cycles

EMERGENCY LIGHT BATTERY PACK M1670 FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW 33-51-06. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,181 hrs · 18,936 cycles

LEFT OVERWING AFT EMERGENCY LIGHT INOP. RELAMPED LEFT OVERWING AFT EMERGENCY LIGHT REF AMM 33-51-04-960- 801. OPS CHECK GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 46,010 hrs · 18,469 cycles

G7 GALLEY AFT EMERGENCY LIGHT LENS IS BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,010 hrs · 18,469 cycles

EMERGENCY LIGHT FEEDER CABLE JUST FWD OF LEFT FWD ESCAPE HATCH AND SEA T 20ABC HAS CHAFED AND PINCHED WIRES. REMOVED THE FEEDER CABLE AND FOUND NO DEFECTS. REINSTALLED THE FEEDER CABLE, OPS CHECK FAILED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-00. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,010 hrs · 18,469 cycles

G7 GALLEY FWD EMERGENCY LIGHT LENS IS BROKEN. REMOVED AND REPLACED THE LIGHT AND REPLACED BATTERY PACK. SYSTEM OPS CHECKED GOOD IAW AMM 33-51-00.

Part: SKIN — DENTED (APU DOOR) · airframe 46,010 hrs · 18,469 cycles

DENT ON SKIN FORWARD APU DOOR HINGE. REPAIRED IAW SRM 53-80-01 REPAIR 1.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 45,512 hrs · 18,268 cycles

EMERGENCY LIGHTS FROM SEAT 8C TO 15C INOPERATIVE. R & R POWER SUPPLY & BATTERY PACK IAW AMM 33-51-06. OPERATIONS NORMAL.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,614 hrs · 16,777 cycles

REF FCD 5510-02451 RT HORIZONTAL STAB IN SPAR RIBS INSPECTION FOUND ONE CRACK AT STAB STATION 92.70, ABOVE TRANSITION RADIUS AT STIFFENER NR 4. INSTALLED STIFFENER REPAIR IAW SRM 55-10-09 REPAIR 4.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,614 hrs · 16,777 cycles

REF FCD 5510-02451 RT HORIZONTAL STAB IN SPAR RIBS INSPECTION FOUND ONE CRACK AT STAB STATION 2.70, ABOVE TRANSITION RADIUS AT STIFFENER 3. INSTALLED STIFFENER REPAIR IAW SRM 55-10-09 REPAIR 4.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,614 hrs · 16,777 cycles

REF FCD 5510-02451 RT HORIZONTAL STAB IN SPAR RIBS INSPECTION FOUND ONE CRACK AT STAB STATION 92.70, ABOVE TRANSITION RADIUS AT STIFFENER 2. INSTALLED STIFFENER REPAIR IAW SRM 55-10-09 REPAIR 4.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,614 hrs · 16,777 cycles

FORWARD CARGO PIT ANTENNA DOUBLER BETWEEN STATION 500 - 500A, LOWER BILGE HAS CORROSION. ALL WORK ACCOMPLISHED IAW ECRA 5331-02010. REPAIR PLACED ON DIP 53, DIP CONTROL 032207. ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 01/30/2017. PLANNING TO CONTACT ENGINEERING AFTER 11/30/2016 BUT BEFORE 12/30/2016 FOR THE PERMANENT REPAIR. NOTE THIS REPAIR UNDER DTA IAW ECRA 5331-02010 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,614 hrs · 16,777 cycles

AD 2009-01-02 RT CABIN AREA FRAME STATION 380 BETWEEN STRINGER 8 & 9 CRACKED IAW EA 5310-04716 OP 3. REPAIRED FRAME AT STATION 380 BETWEEN STRINGER 8R & 9R IAW EA 5310-04716 REV H OP 3. ALL TASK & WIPS FOR PARTIAL WORKED ACCOMPLISHED.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 41,614 hrs · 16,777 cycles

FOUND CRACK AT LT HORIZONTAL STAB LOWER SKIN AT STATION 97 REAR SPAR. ADDITIONAL SKIN CRACKS FOUND ON LOWER INSPAR SKIN AT STAB STATION 101.90, 28 IN AFT OF LE & STATION 101.50 10 IN FWD OF RS. THE NEW DOUBLER WILL ENCOMPASS ALL 3 REPAIR AREAS IAW SRM 55-10-01 REPAIR 11 REF NR 9984340 & 9715825. INSPECTION AT 56,000 FLIGHT CYCLES AFTER REPAIR & REPEAT EVERY 9000 FLIGHT CYCLES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,614 hrs · 16,777 cycles

AD 2009-01-02 RT CABIN AREA FRAME STATION 400 BETWEEN STRINGERS 8 & 9 CRACKED IAW EA 5310-04716 OP 3. REPAIRED FRAME IAW EA 5310-04716 OP 3. SEE ALL TASKS & WIPS FOR PARTIAL WORK ACCOMPLISHED.

Part: CONNECTOR — SHORTED (WHEEL WELL) · airframe 40,645 hrs · 16,362 cycles

WHEEL WELL FIRE AFTER TAKEOFF FOUND CONNECTOR D840 SHORTED. INSTALLED NEW CONNECTOR D84 IAW SWP 20-62-14. PERFORMED WW FIRE TEST, OPERATIONS CHECKED GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 38,429 hrs · 15,525 cycles

EXIT SIGN AT 2R FALLING OFF. R & R R2 DOOR L1191 EMERGENCY EXIT SIGN IPC 3 3-51-01-06F. EMERGENCY LIGHT TEST PASSED AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RIGHT EMERGENCY EXIT LIGHT (EXTERIOR) BS 608 IS INOPERATIVE. REPLACED BATTERY PACK AT M1676, IAW AMM 33-61-12.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,506 hrs · 14,783 cycles

RT FWD OVERWING EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. PERFORMED OPS CHECK IN REF WITH MM 33-51-00, CHECKED GOOD. R & R BATTERY PACK IAW MM 33-51-12.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 34,571 hrs · 14,017 cycles

LEFT LOWER HORIZONTAL STAB SKIN IS CRACKED AT STAB STA 101.50 AND 10" FWD OF REAR SPAR INSTALLED REPAIR DOUBLER AND FILLER REF SRM 55-10-01, REPAIR 11.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,353 hrs · 12,740 cycles

DURING RON CHECK, FOUND SEAT MOUNTED EMERGENCY LTS FROM 22ABC - 26ABC INOP. FOUND POWER SUPPLY BAD. REMOVED & REPLACED POWER SUPPLY ASSY REF AMM 33-51-06-960-806. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,550 hrs · 12,034 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED, OPS CHECKS GOOD.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,339 hrs · 11,551 cycles

SUPPORT TASK. RT HORIZONTAL STAB HAS A .75 INCH LONG CRACK IN THE LOWER SKIN STAB STA 101.9 I/B SIDE OF RIB, 8 INCH AFT OF DRAIN HOLE AND 10.5 INCH FWD OF AFT EDGE OF SKIN PANEL REPAIRED CRACK ON RT HORIZONTAL STAB PER ECRA#5510-02120. PLACED ON DIP TO ACCOMPLISH AN INITIAL INSPECTION PRIOR TO 20,551 TOTAL AIRCRAFT CYCLES AND THEN REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 9,000 FLIGHT CYCLES PER PART 2 OF ECRA 5510-02120 "Q/C" IF ANY DEFECTS ARE NOTED CONTACT ENGINEERING FOR "Q/C" ACCOMPLISH AN INITIAL INSP PRIOR TO 20551 TOT FLT CYCLES DISPOSITION. DIP C/N 07015 ISSUED. AND THEN REPEAT INSP AT INT NOT TO EXCEED 9000 FLT CYCLES PER PART 2 OF EC5510-02120. PERFORM A D/V INSP OF THE (-1) REPAIR DOUBLER FOR DEFECTS. PERFORM LFEC INSP OF THE SKIN UNDERNEATH THE (-1) REPAIR DOUBLER PER NDT MANUAL PART 6 53-30-00 FIG.5 1) INIT: W/I 20551 TOTAL A/C F/C. INIT WILL AUTO-ITO TO 2) RIR: W/I EVERY 9000 F/C THEREAFTER (M&E 59-9955-8-0141).

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,339 hrs · 11,551 cycles

SUPPORT TASK. RT HORIZONTAL STAB HAS A 1" LONG CRACK IN THE LOWER SKIN STAB STA 101.9 I/B SIDE OF RIB. 27.5" AFT OF L/E OF SKIN PANEL AND 19.5" FWD OF AFT EDGE OF SKIN PANEL REPAIRED CRACK ON R/H HORIZONTAL STAB AND DAMAGED RIB PER ECRA# 5510-02120. PLACED ON DIP TO ACCOMPLISH AN INTIAL INSPECTION PRIOR TO 20,551 TOTAL AIRCRAFT CYCLES AND THEN REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 9,000 FLIGHT CYCLES PER PART2 OF ECRA#5510-02120 "Q/C" PERFORM A LFEC INSP OF THE SKIN UNDERNEATH THE (-1) "Q/C" ACCOMPLISH AN INTIAL INSP OF THE R/H HORZ STAB LWR SKIN REPAIR DOUBLER PER NDT MANUAL PART 6 53-30-00 FIG. 5 AND REPAIR DOUBLER PRIOR TO 20551 TOT FLT CYCLES AND THEN REPEAT ENSURE THAT THERE ARE NO DEFECTS. IF ANY DEFECTS ARE NOTED INSP AT INTERVALS NOT TO EXCEED 9000 FLT CYCLES PER PART 2 OF CONTACT ENGINEERING FOR DISPOSITION. DIP C/N 07016 ISSUED. EC5510-02120. PERFROM A D/V INSP OF THE (-1) REPAIR DOUBLER FOR DEFECTS. PERFROM LFEC INSP OF THE SKIN BENEATH THE (CONTINUED) 1) INIT: W/I 20551 TOTAL A/C F/C. INIT WILL AUTO-ITO TO 2) RIR: W/I EVERY 9000 F/C THEREAFTER (M&E 59-9955-8-0143)-ODEE

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,543 hrs · 9,772 cycles

FLIGHT DECK PANEL JUST UNDER COCKPIT DOOR, CENTER INTERCOSTAL SUPPORT HAS HEAVY CORROSION. REPLACED CENTER INTERCOSTAL (FLOOR STEP) PER ECRA 5321-01611 REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,543 hrs · 9,772 cycles

FLOORBEAM UPPER SURFACE AREA HAS CORROSION (PITTED) STATION 986.5 AND RBL 23. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER SRM 53-00-51, FIGURE 203, REPAIR 1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,543 hrs · 9,772 cycles

FORWARD ENTRYWAY INTERCOSTAL LOCATED BETWEEN FLOORBEAMS STATIONS 312 AND 328, LBL 45 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL AT STATION 312 - 328, LBL 45 PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,543 hrs · 9,772 cycles

FORWARD ENTRYWAY INTERCOSTAL LOCATED BETWEEN FLOORBEAMS STATIONS 312 AND 328, RBL 31 CRACKED AT FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL AT STATIONS 312 - 328, RBL 31 PER SRM 51-40-02.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,272 hrs · 9,267 cycles

RIGHT FORWARD EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED RIGHT FORWARD EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM TASKS 33-51-06-960-805 AND 33-51-06-960-806, OPERATION CHECKS NORMAL.