N69826

Part: GUIDE ARM — LACK OF LUBE (ZONE 800) · airframe 34,656 hrs · 12,702 cycles

MAIN CAB DOOR LIGHT ON DURING TAXI POST LANDNG CLEANED/GREASED GUIDE ARM AREAS REF AMM 52-11-21-400-802 AND AMM 12-25-11-640-801. OPEN AND CLOSED DOOR WITH NO FAULTS FOUND. LIGHT TURNED ON AND OFF WHEN COMMANDED

Part: TIRE — FAILED (ZONE 700) · airframe 31,596 hrs · 11,487 cycles

MAIN LANDING GEAR TIRE FAILURE ON DEPARTURE FROM DENVER UPON ARRIVAL FOUND NO.3 MLG TIRE BURST. SEE PICTURES. REMOVED AND REPLACED NO.3 MLG TIRE IN REFERENCE AMM 32-45-11/401.

Part: CABLE — INTERFERENCE (AFT CARGO DOOR) · airframe 29,882 hrs · 10,834 cycles

AFT CARGO DOOR LT ON TAKEOFF. REJECTED TAKEOFF AT 40 KTS DUE TO AFT CARGO DOOR INDICATION. PERFORMED OPERATIONAL CHECK OF AFT CARGO DOOR FOUND DOOR BUNGE CABLE COUGHT ON ONE OF THE DOOR STOPS OPS. OPEN AND CLOSE DOOR SEVERAL TIMES LIGHT EXTINGUISHED OPS CHECK NORMAL. AMM TASK 52-00-00-210-801.

Part: BATTERY PACK — INOPERATIVE (M2626) · airframe 28,255 hrs · 10,201 cycles

BATTERY PACK M2626, LIGHTS SHUT OFF PRIOR TO 15 MINUTES MINIMUM (REF. AAR NR 99976128). REPLACED BATTERY PACK M2626 OF EMERGENCY LIGHT AT PASSENGER CABIN IAW B737 AMM 33-51-06-960-805, OPS CHECK GOOD (SDR # 1033516) (WORK ACCOMPLISHED BY V943433 AND AAR QC A-83 V935067).

Part: BATTERY PACK — INOPERATIVE (M2627) · airframe 28,255 hrs · 10,201 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M2627 FAILS OP CHECK (REF. AAR NR 99981055). REPLACED BATTERY PACK M2627 OF EMERGENCY LIGHT AT PASSENGER CABIN IAW B737 AMM 33-51-06-960-805, OPS CHECK GOOD (WORK ACCOMPLISHED BY V943433 AND AAR QC A-83 V935067) SDR# 1033518.

Part: BATTERY PACK — INOPERATIVE (M7694) · airframe 28,255 hrs · 10,201 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M1694 FAILS OP CHECK (REF. AAR NR 99981056). REPLACED BATTERY PACK M1694 OF EMERGENCY LIGHT AT PASSENGER CABIN IAW B737 AMM 33-51-06-960-805, OPS CHECK GOOD (SDR #1033517) (WORK ACCOMPLISHED BY V943433 AND AAR QC A-83 V935067).

Part: BATTERY PACK — INOPERATIVE (M2816) · airframe 28,255 hrs · 10,201 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M2816 FAILS OP CHECK (REF. AAR NR 99981057). REPLACED BATTERY PACK M2816 OF EMERGENCY LIGHT AT PASSENGER CABIN IAW B737 AMM 33-51-06-0960-802, OPS CHECK GOOD (SDR # 1033515) (WORK ACCOMPLISHED BY V943433 AND AAR QC A-83 V935067).

Part: HMU — FAULTY (ENG #1) · airframe 26,936 hrs · 9,706 cycles

RTO BELOW 80 KTS DUE TO 1 ENGINE NOT PRODUCING REQ. THRUST WITH A/T AND MANUAL MONITORING CHANGES TO REGULATOR -9. REF FIM 73-05-TASK808, ACPD #1 ENG EEC BITE, NO FAULTS NOTED, ACPD #1 ENG EEC ACT TEST, NO FAULTS, STARTED #1 ENG-IDLE, HAD REGULATOR 9 ON INPUT MONITORING AT FIRST MINUTE THEN CHANGED TO REGULATOR 3, PUSHING #1 ENG THROTTLE JUST ABOVE IDLE - INPUT ADD EMP:U264492 REMOVED & REPLACED #1 ENGINE HMU. IDLE RUN PERFORMED. QTY LEAK & OPS CHECK GOOD. ACPD TEST 5 PWR ASSURANCE CHECK #1 ENGINE. TO INCLUDE UP TO TKO PWR, ALL PARAMETERS IN NORMAL RANGE WITH THROTTLES MATCHED. NO FAULTS DETECTED ON #1 EEC BITE, NO LEAKS NOTED ON ENGINE RUN. PARTS USED: 29-7321-3-0017,QTY 29-7321-9-0012,QTY :1 ADD EMP:U027741,U390982 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1765897 SN OFF 6895 TT # 1851497 SN OFF 0855 PUMP, MAIN FUEL OFF 29-7311-9-0001 6895 ON 29-7311-9-0001 7000 UNIT, HYDROMECH OFF 29-7321-9-0012 0855 ON 29-7321-9-0012 6015

Part: STATIC PORT — SCRATCHED (LEFT) · airframe 21,205 hrs · 7,599 cycles

SURFACE SCRATCH ON L/H ALT STATIC PORT. ON AAR NR 99905149 BLENDED AREA @ L/H ALT STATIC PORT ZONE B ORIGINAL MAT 0.080 ALLOWABLE MAT LOSS 0.005 MAT LOSS 0.002, MAT REMAINING 0.078 ZONE C ORIGINAL MAT 0.080, ALLOW MAT LOSS 0.008 MAT LOSS 0.002 MAT REMAINING 0.078 FOUND TO BE WITHIN LIMITS IAW B737-900 SRM 53-30-01 TABLE 101. WORK ACCOMPLISHED BY V931821 & QC V890739

Part: STATIC PORT — DAMAGED (RT FWD) · airframe 21,205 hrs · 7,599 cycles

SMALL CHIP ON R/H F/O STATIC PORT. ON AAR NR 99905151 BLENDED AREA @ R/H F/O STATIC PORT SKIN ZONE A ORIGINAL MAT 0.080, ALLOWABLE MAT 1055 0.003 MAT 1055 0.001, MAT REMAINING 0.079 FOUND TO BE WITHIN LIMITS IAW B737-900 SRM 53-30-01 TABLE 101. WORK ACCOMPLISHED BY V931821 AND AAR QC V890739

Part: STATIC PORT — SCRATCHED (RT AFT) · airframe 21,205 hrs · 7,599 cycles

SCRATCHES ON R/H ALT STATIC PORT. ON AAR NR 99905152 BLENDED AREA @ R/H ALT STATIC PORT SKIN ZONE B ORIGINAL SKIN 0.090, ALLOW MAT LOSS 0.005, MAT LOSS 0.002, MAT REMAINING 0.088, ZONE C ORIGINAL MAT 0.090, ALLOW MAT LOSS 0.009, MAT LOSS 0.002, MAT REMAINING 0.088 FOUND TO BE WITHIN LIMITS IAW B737-90 0 SRM 53-30-01 TABLE 101 WORK ACCOMPLISHED V931821 & QC V890739

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 21,205 hrs · 7,599 cycles

SURFACE SCRATCH ON L/H CAPT STATIC PORT. ON AAR NR 99905150 BLENDED AREA @ L/H CAPT STATIC PORT SKIN ORIGINAL MAT 0.080 ALLOWABLE MAT LOSS .003, MAT LOSS 0.002, MAT REMAINING 0.078 FOUND TO BE WITHIN LIMITS IAW B737-900 SRM 53-30-01 TABLE 101.

Part: CHARGER — INOPERATIVE (MASTER) · airframe 16,039 hrs · 5,684 cycles

BATTERY DISHAGE LIGHT CAME ON. RETURNED SHOWED 4 TO 8 DISCHG UN TIL LANDING REMOVED AND REPLACED MAIN BATTERY REF AMM 24-31-11-400-801-001.O PS CK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1296306 SN OFF 6302 BATTERY, AIRCRA OFF 29-2431-9-9001 6302 ON 29-2431-9-9001 0892 PRE-CAUTIONARY RMV. & RPLC. MAIN BATT. CHARGER REF. AMM 24-31- 21. OPS C/K ON MAIN BATT. CHRGR. GOOD REF. AMM 24-31-21-710- 801. HANGAR MAINT. PERFORM ENGINE RUN WITH NO DEFECTS NOTED. O.K. FOR SVC. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1871695 SN OFF 1765 CHARGER, BATTER OFF 29-2431-9-0002 1765 ON 29-2431-9-0002 2940

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 13,439 hrs · 4,771 cycles

FLOOR EMERGENCY LIGHT LENS CRACKED, AFT OF THE FWD CLOSET, FWD OF SEAT 1B. REPLACED THE LENS.

Part: COVER — LOOSE (DOOR SLIDE) · airframe 13,038 hrs · 4,622 cycles

ESCAPE SLIDE IS FALLING OUT OF ITS HOLDER. REINSTALLED THE BUSTLE IN SLIDE PACK COVER, INSPECTED SLIDE FOR DEFECTS, DISENGAGED GIRT BAR & INSTALLED IN THE HOLDER ON SLIDE PACK COVER & FLOOR TRACK OPS CHECKED GOOD.

Part: SLIDE — PARTIAL DEPLOY (1L DOOR) · airframe 11,633 hrs · 4,118 cycles

L1 DOOR NOT DISARMED PRIOR TO OPENING.SLIDE PACK PARTIALLY DEPLOYED. FOUND L1 MAIN DOOR SLIDE PACK FALLEN AND TRAPPED AGAINST FLOOR WITH GIRT BAR INSTALLED. PERFORMED ESCAPE SLIDE RENDER SAFE CHECKLIST IAW GMM 02-30-25. REMOVED AND INSPECTED SLIDE PACK AND SUPORT ASSY. INSTALLED ESCAPE SLIDE PACK IAW AMM TASK 25-66-0 1-400-801. ACFT GOOD TO CONTINUE SERVICE. ESCAPE SLIDE L1 INSTALLED IAW AMM 25-66-01-400-801.

Part: HANGER ASSY — OUT OF ADJUST (R1 GIRT BAR) · airframe 11,596 hrs · 4,105 cycles

FA REPORTED THE R1 DOOR SLIDE GIRT BAR HARD TO SET. ADJUSTED THE GIRT BAR HANGERS. OPS CHECKED NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,181 hrs · 3,954 cycles

ALL EMERGENCY LIGHTS WILL NOT SHUT OFF IN ARMED OR OFF. RESET AIRCRAFT POWER. ALL EMERGENCY LIGHTS NORMAL.

Part: WIRE — EXPOSED (CABIN) · airframe 10,595 hrs · 3,739 cycles

SEAT 1B FLOOR PROXIMITY/EMERGENCY ESCAPE PATH LIGHT HAS BARE WIRES STICKING OUT INTO AISLE. SEAT 5B (SAME LIGHT) HAS LENS MISSING AND BOTH BULBS BROKEN. RPL'D LIGHT ASSY ON 1B AND 5B, OP CK'S NORMAL.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 10,548 hrs · 3,725 cycles

1R SLIDE DIFFICULT TO DISARM. ADJUSTED GIRT. OPS CKS OK REF AMM 25-66-01

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 177 hrs · 67 cycles

SUPPORT TASK AISLE LIGHTING FROM ROW 22ABC TO 25ABC INOPERATIVE, TROUBLESHOOTING. REMOVED LOWER SIDEWALL PNL AT ROW 27ABC FOR ACCESS TO CONNECTOR D14710, FOUND IT WAS NOT SEATED PROPERLY. RESEATED CONNECTOR D14710 IAW SWPM 20-60-06 AISLE LIGHTS. CHECKED GOOD IAW AMM 33-51-11.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 171 hrs · 65 cycles

SPT OVER WING EMER LIGHTS RT SIDE INOPERATIVE. R & R LAMP IAW AMM 33-51-04-960-801. OPERATIONS CHECKED GOOD IAW AMM 33-51-04-960-801.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

OVERWING EMERGENCY EVACUATION LIGHTS ARE INOP. REMOVED AND REPLACED OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY IAW MM 33-53-00. OPS CHECK GOOD.

Part: POWERPACK — MALFUNCTIONED (RUDDER) · airframe 44,667 hrs · 22,125 cycles

DECENT INTO IAH, AT 10,000 FEET, 250 KNOTS, LOUD RUMBLE OCCURED WITH SPEED BRAKE STOWED ACCOMPANIED BY SHARP ROLL RIGHT. EMERGENCY DECLARED. LANDED IN IAH UNEVENTFUL. REMOVED AND REPLACED RUDDER POWER PACK IAW MM 272008. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (#2 GALLEY) · airframe 44,400 hrs · 21,999 cycles

INSPECTION FOUND R/H O/B SEAT TRACK CORRODED AT GALLEY MOUNT FOR #2 GALLEY. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE 4F.

Part: FRAME — CRACKED (STA 1463) · airframe 44,398 hrs · 21,998 cycles

INSPECTION FOUND A 1" CRACK IN CANTED FRAME AT STA 1463, L3L-L3R. THE CRACKED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-00 AND 51-30-05.

Part: CLIP — OUT OF ADJUST (TAILCONE) · airframe 44,398 hrs · 21,998 cycles

THE FORCE REQUIRED TO PULL EXTERIOR TAIL CONE RELEASE HANDLE FROM ITS RETAINING CLIPS EXCEEDED 35 POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND PULL WAS WITHIN LIMITS AT 25 POUNDS.

Part: LANYARD · airframe 43,626 hrs · 21,573 cycles

AFT GALLEY SLIDE LANYARD IMPROPERLY INSTALLED AT PREVIOUS STATION BY A CREWMEMBER. REPORTED BY FLIGHT ATTENDANT. REINSTALLED LANYARD PER 25-62-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 41,434 hrs · 20,418 cycles

INSPECTION FOUND FUSELAGE SKIN CREASED JUST BELOW CUSP LINE AT STA 408-446. A REPAIR WAS INSTALLED IAW ECRA 5310-04154 AND SRM 53-04, FIGURE 12B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,434 hrs · 20,418 cycles

INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 1041-1322. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01.

Part: WIRE — BURNED (COCKPIT) · airframe 39,417 hrs · 19,319 cycles

AFTER APPROXIMATELY 15 MINUTES OF LEVEL FLIGHT AT FL310 COCKPIT FILLED WITH SMOKE. POPPING AND SPARKING OCCURRED AT THE JUMP SEAT (OBSERVERS) RT SHOULDER AREA. FOUR AC BUS CIRCUIT BREAKERS POPPED BEHIND CAPTAINS SEAT. AIRCRAFT DIVERTED TO BHM. FOUND 15 WIRES DAMAGED TO AC POWER SYSTEM (REF W/D 34-51-01). REPLACED ALL DAMAGED WIRES PER 20-00-13 AND 20-10-03. REPLACED 6 LT AC BUS BREAKERS AND 6 RT AC BREAKERS AS PRECAUTION. DAMAGE TO WIRES CAUSED BY CHAFING ON SCREW. POWERED UP AC ELECTRICAL SYSTEM. CHECKS NORMAL.

Part: BALANCE WT — CORRODED (RT ELEVATOR)

INSPECTION FOUND RT ELEVATOR O/B TIP MASS BALANCE CORRODED. THE RT WEIGHT WAS REMOVED. INSTALLED NEW RIB AND COUNTER WEIGHT IAW SRM 51-30-05.

Part: SKIN — DENTED (LT ELEV TRIM TAB)

INSPECTION FOUND THE LT ELEVATOR GEAR TRIM TAB DENTED AT I/B TRAILING EDGE. THE TRIM TAB WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 27-30-04.

Part: SKIN — DENTED (BS 229-265)

INSPECTION FOUND DENTS IN FORWARD FUSELAGE SKIN ABOVE CUSP LINE AT FS 229 - 265, LONGERON 15L - 18L. THE DENTED AREA OF SKIN WAS REMOVED, A NEW SECTION OF SKIN, DOUBLER, AND LONGERON STRAP WERE INSTALLED IAW SRM 51-10-03 AND ECRA 5330-02445.

Part: LONGERON — CRACKED (BS 1418)

INSPECTION FOUND A 1 INCH CRACK IN LONGERON 2R AND A 1 INCH CRACK IN LONGERON 2L AT STA 1418. BOTH SECTIONS OF CRACKED LONGERON WERE REMOVED AND REPLACED WITH SPLICE IAW SRM 53-02, FIGURE 18.

Part: FRAME — CRACKED (BS 1418)

INSPECTION FOUND A .5 INCH CRACK ON BELTFRAME STA 1418 UNDER LONGERON 2L AND A 1 INCH CRACK AT LONGERON 2R. THE CRACKS WERE STOP DRILLED AND REPAIRS WERE INSTALLED IAW DOUGLAS SERVICE REWORK DRAWING SR09530003.

Part: INTERCOSTAL — CRACKED (PAX DOOR)

INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.

Part: ANGLE — CORRODED (BAGGAGE COMPT)

INSPECTION FOUND Z-ANGLE CORRODED ALONG ENTIRE LENGTH OF LOWER DOOR JAMB IN AFT BAGGAGE BIN. THE ANGLE WAS REPAIRED IAW SRM 53-05, FIGURE 63.

Part: SLIDE — LOW PRESSURE (TAILCONE)

INSPECTION FOUND AFT TAILCONE SLIDE BOTTLE PRESSURE LOW. THE TAILCONE SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-02.

Part: BEARING — FAILED (NR 2 ENGINE)

THE NR 2 ENGINE FAILED WHILE EN ROUTE FROM IAH TO TUS. A MUFFLED BANG WAS HEARD WITH THE EPR AND RPM DROPPING TO ZERO. THE AIRCRAFT WAS DIVERTED TO ELP WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP TEARDOWN FINDINGS REVEALED FAILURE OF UPPER TOWER SHAFT BEARING.

Part: BELT FRAME — CORRODED (BS 1309)

HOU - INSPECTION FOUND BELT FRAME CORRODED AT STA 1309, LONGERON 27L TO LONGERON 27R. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED AND PRIMED IAW SRM 53-01. (X)

Part: RIB — CRACKED (RT WING)

HOU - INSPECTION FOUND A 3 INCH CRACK IN RT WING RIB. A DOUBLER WAS INSTALLED IAW SRM 57-06, FIGURE 5. (X)

Part: RIB — CRACKED (NR 9 FLAP TRACK)

HOU - INSPECTION FOUND A 1 INCH CRACK AT LOWER FLANGE OF FOURTH RIB OUTBOARD OF NR 9 FLAP TRACK. A NEW RIB WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-30-5. (X)

Part: DOUBLER — CRACKED (WS 194.843)

HOU - INSPECTION FOUND A 2 INCH CRACK IN SPLICE DOUBLER AT LEADING EDGE STATION 194.843. THE SPLICE DOUBLER WAS REPAIRED IAW ECRA 5710-01645. (M)

Part: SKIN — DENTED (BS 1193)

HOU - INSPECTION FOUND A 1 INCH LONG DENT IN SKIN AT STA 1193, LONGERON 19L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 21. (X)

Part: ANGLE — CORRODED (FWD BAGGAGE BIN)

HOU - INSPECTION FOUND THRESHOLD Z-ANGLE CORRODED IN FORWARD BAGGAGE BIN. THE AREA WAS REPAIRED IAW SRM 53-01 AND SRM 51-10-1. (X)

Part: SLIDE — LOW PRESSURE (GALLEY DOOR)

IAH - FLT 0291 - INSPECTION FOUND THE AFT GALLEY DOOR EMERGENCY EVACUATION SLIDE WITH LOW PRESSURE DURING A PRE-FLIGHT CHECK. THE AFT GALLEY DOOR EMERGENCY EVACUATION SLIDE WAS REMOVED AND REPLACED. (X)