N999DN

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 72,182 hrs · 52,460 cycles

CRACK FOUND ON FWD LEFT HAND LANDING GEAR DOOR FRAME. REPLACED LT INB MLG DOOR ASSY PER MD88 AMM 32-12. DOOR, MLG, LH S OFF 92-3210-9-0005 S/N 00092. (LP6629878)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,182 hrs · 52,460 cycles

LT AND RT FWD OVERWING EMER LIGHT INOP. FOUND NO POWER AT L2-177 AND L2-176. 503183. REPLACED BATTERY PACK AT B5-103 PER MD AMM 33-50. (LP6629877)

Part: BATTERY — MISSING (LAV SMOKE DETECT) · airframe 72,030 hrs · 52,308 cycles

LAVATORY SMOKE DETECTOR BATTERY MISSING. REPLACE DETECTOR BATTERY. OPS NORMAL POSITION AFT LEFT LAV. (LP1359607)

Part: SUPPORT ANGLE — CRACKED (TAILCONE) · airframe 71,909 hrs · 52,194 cycles

TAIL CONE UPPER R/H LOCK SUPPORT ANGLE CRACKED. REMOVED UPPER R/H LOCK SUPPORT BRACKET. (334965) REINSTALLED UPPER R/H LOCK SUPPORT BRACKET PER MD88 DWG 5966796. (LP1330971)

Part: SUPPORT FRAME — CRACKED (TAILCONE) · airframe 71,909 hrs · 52,194 cycles

TAILCONE SUPPORT FRAME CRACKED @ 3:00 MKD. RMVD TAIL CONE SUPPORT FRAME RT SIDE AT 3:00 (190190) STARTED PICKING UP HOLES ON THE FACE OF THE FRAME. (190190) INSTALLED FRAME SPLICES, CLIPS, BRACKETS AND SUPPORT STRUCTURE PER MD988 DWG 5966796 (416230) FINISHED INSTALL OF FRAME PER MD88 DWG 5966796(416230) (LP1330969)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,144 hrs · 51,501 cycles

2L EMERGENCY EXIT COVER DIFFUSER LENS MISSING. MAINTENANCE REINSTALLED COVER, OK FOR SERVICE.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 71,144 hrs · 51,501 cycles

IFSD & ATB - THE CREW RETURNED THE AIRCRAFT BACK TO DEPARTURE FOLLOWING THE FAILURE OF THE #1 ENGINE. THE LEFT ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF, WITH THE EGT REACHING 800 DEGREES, AND THEN THE #1 ENGINE ROLLED BACK. THE ENGINE WAS SHUT DOWN AND SECURED BY THE FLIGHT CREW PER THE QRH. : MAINTENANCE REPLACED ENGINE.

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE) · airframe 70,737 hrs · 51,150 cycles

AFTER TAKEOFF AND DURING CLIMB- B/W 8-10K L INLET FUEL PRESS. LO ILLUMINATED ON EOAP. RAN QRH- 12.22- ONCE ALL PUMPS WERE ON, ONLY 150LB. OF FUEL IN CENTER AT THAT TIME. L INLET FUEL PRESS. LO LIGHT (EXT.).- NOTICED FWD. LEFT FUEL TANK BOOST PUMP CB (J23) POPPED. DURING FURTHER CLIMB FL240-260, L INLET FUEL PRESSURE LO LIGHT REILLUM. WENT BACK TO QRH. 12.22- THEN TO 12.13. FUEL IMBALANCE NOW AT 900 LBS B/W L MAIN/R MAIN TANK. CTR. TANK 50LBS. LEFT ENG. BEGAN TO SURGE WITH POWER- RT, ENG. STEADY 1.38- LT. ENG. EPR 1.26- 1.05- 1.58. N1 ROLLING UP AND DOWN. AUTO THROTTLES WERE ENGAGED. ENG. ANTI ICE WAS ALSO ON. YOU COULD FEEL THE LARGE POWER CHANGES THROUGHOUT THE CABIN. AT WERE DISCONNECTED. AND LEFT ENGINE POWER WAS BROUGHT DOWN TO IDLE POWER. SURGES IN POWER NO LONGER OCCURRED. OIL PRESSURE WAS STABLE AND NORMAL. NO SEVERE DAMAGE WAS SUSPECTED. EMERGENCY DECLARED AND RETURN BACK TO DEPARTURE. NORMAL LANDING. PER MCC REQUEST, DISCONNECTED MAIN FUEL LINE AND INSPECTED FOR OBSTRUCTION. FUEL LINE FOUND TO BE CLEAR AT DISCONNECTION AND RECONNECTED MAIN FUEL LINE. REMOVED MAIN FILTER FOR FUEL PUMP. FOUND FILTER CONTAINING SOME TRASH BUT NOT SIGNIFICANT. REPLACED FUEL PUMP MAIN FILTER IAW MD88 AMM 73-12. .REPLACED FUEL CONT. FILTER IAW MD88 AMM 73-12, BORO'D ENG. FUEL FEED LINE. NO OBSTRUCTIONS FOUND; INSP'D ENG INLET AND EXHAUST, NO DEFECTS NOTED. RAN ENG. IAW AMM 71-00. ENG. RAN SMOOTH AT ALL SPEEDS; PARAMETERS NML. PERF. FUEL HEAT CK., OIL TEMP RISES PROPERLY. PERF. ACCEL CK, CKS GOOD.LEAK CK. GOOD.(477612). RMVD. LT. ENG. FUEL CONTROL AND STARTED INSTALL OF NEW ONE IAW MD88 AMM 73-20. COMPLETED INSTALL OF NEW FUEL CONTROL IAW MD88 AMM 73-20. PERFORMED ENG. TRIM IAW MD88 AMM 71-00. RAN ENG. TO TAKEOFF POWER. NO ABNORMALITIES NOTED. ALL PARAMETERS STEADY. MAIN FUEL FILTER LEAK CK GOOD. (LP5672100)

Part: SLIDE — DAMAGED (L;1 DOOR) · airframe 70,645 hrs · 51,072 cycles

L1 DOOR GIRT BAR HUNG ON DOOR FRAME. FOUND SLIDE PACK DAMAGED DID NOT DEPLOY. REPLACED L1 DOOR SLIDE PACK PER 2561-01358-01A. SLIDE, EVAC, FO OFF 97-2561-9-0003 02768 ON 88-2560-9-0003 03673. (LP5813124)

Part: DETECTOR — MISSING (NLG) · airframe 70,510 hrs · 50,952 cycles

LT NOSE DEBRIS DEFLECTOR MISSING. INSTALLED LEFT NOSE GEAR DEBRIS DEFLECTOR PER MD88 AMM 32-20. (LP5738614)

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 69,623 hrs · 50,184 cycles

EMERGENCY EXIT LIGHTS ROWS 29&30 INOP. FOUND LIGHTS UNPLUGGED, RESECURED PLUGS, OPS CK GOOD. (LP4764612)

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 68,803 hrs · 49,487 cycles

WEAR ON LOWER SKIN OF RT/FWD OVERWING EMERGENCY EXIT DOOR JAMB. IN REF NRC 00086 WEAR ON LOWER SKIN OF RT/FWD OVERWING EMERGENCY EXIT DOOR JAMB WAS REPAIRED PER ETI-88-17-054 REV 4 AND ER/A 569086-14 REV ORG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,803 hrs · 49,487 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB. CORROSION LEVEL 2. CORROSION ON AFT CARGO COMPARTMENT DOOR JAMB WAS REPAIRED PER SRM 53-05 FIG 123. AREA WITHIN LIMITS WAS ATTENDED WITH NRC 00211.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 68,803 hrs · 49,487 cycles

WEAR ON LOWER SKIN OF RT/FWD OVERWING EMERGENCY EXIT DOOR JAMB. IN REF NRC 00086. WEAR ON LOWER SKIN OF RT/FWD OVERWING EMERGENCY EXIT DOOR JAMB WAS REPAIRED PER ETI-88-17-054 REV 4 AND ER/A 569086-14 REV ORG. PERFORM GENERAL VISUAL INSPECTION OF THE SECTION I REPAIR . PER ERA 569086-14 REV ORIGINAL SECTION II UNDER LOG 0579816.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 68,803 hrs · 49,487 cycles

WEAR ON LOWER SKIN OF RT/FWD OVERWING EMERGENCY EXIT DOOR JAMB. WEAR ON LOWER SKIN OF RT/FWD OVERWING EMERGENCY EXIT DOOR JAMB WAS REPAIRED PER ETI-88-17-054 REV 4 AND ER/A 569086-14 REV ORG.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 68,770 hrs · 49,465 cycles

ON SERVICE CK FOUND FIRST CLASS EMERGENCY ESCAPE LIGHT ON SEATS INOP. REMOVED AND REPLACED POWER SUPPLY IN FIRST CLASS AREA. OPS CKS GOOD PER AMM 33-50.

Part: SLIDE — LOW PRESSURE (TAILCONE) · airframe 68,637 hrs · 49,361 cycles

TAIL CONE SLIDE NEEDLE IN RED BEYOND LIMITS. REMOVED AND REPLACED AFT TAIL CONE SLIDE.

Part: WIRE — PULLED (CONNECTOR) · airframe 68,497 hrs · 49,255 cycles

AFT EMERGENCY LIGHTS IN TAIL INOP. REMOVED AND REPLACED BATTERIES IN BATT PACK, FOUND PULLED WIRE FROM CANNON PLUG AT WALL CONNECTION. REINSTALLED WIRE AT CONNECTOR AND LIGHT. OPERATIONAL CHECK OK IAW AMM 33-50.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,450 hrs · 49,222 cycles

OVERHEAD EMERGENCY LIGHTS AT ROWS 11-13 INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS FUNCTIONED NORMALLY.

Part: DOOR FRAME — DELAMINATED (FUSELAGE) · corrosion level 2 · airframe 68,121 hrs · 48,978 cycles

FOUND SEVERE DELAM CORROSION. AFT RT CORNER OF AFT LAV SVC DOOR FRAME. COMPLIED WITH ERA 482821-14 REV A. RECEIVED FINAL ERA 48281-14 REV A. COMPARED TO PRI 482821-14 REV A. REV 2. PRI MATCHES ERA.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,126 hrs · 48,983 cycles

CORROSION FOUND ON THE EXTERNAL DOUBLER, AROUND THE AFT LAVATORY WASTE SERVICE PANEL. THE DOUBLER WAS REPLACED IAW ER/A 482821-14, REV ORIGINAL, REVISION A.

Part: CONNECTOR — DEFECTIVE (LT ENGINE) · airframe 67,708 hrs · 48,664 cycles

DIVERTED TO TPA DUE TO A LEFT ENGINE OIL STRAINER CLOG MESSAGE. MAINTENANCE CHECKED THE FILTER AND CHIP DETECTOR AND FOUND NO DEBRIS. THE INDICATION WAS DEFERRED TO MEL. MAINTENANCE WORKING THE MEL PERFORMED WIRING CHECKS AND FOUND NO TROUBLE. THE CONNECTOR FOR THE DELTA P SWITCH WAS FOUND IN POOR CONDITION AND REPLACED. THE DIFFERENTIAL PRESSURE SWITCH WAS ALSO REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SELECTOR SWITCH — SHORTED (WATER QTY) · airframe 66,674 hrs · 47,869 cycles

SMOKE CAME FROM ROW 1DC LOWER WALL VENT. ON ACFT POWER UP. FOUND WATER QUANTITY MODE SELECTOR SWITCH SHORTED. REPLACED FILL VENT VALVE (M1-75). ALL CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 66,090 hrs · 47,429 cycles

ROW 11E EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRES AT THE CONECTOR. REPAIRED THE WIRES IAW ESPM 90-03.

Part: ENGINE — VIBRATION (LEFT) · airframe 65,961 hrs · 47,348 cycles

AIRCRAFT LEVELED AT 370 AND POWER RETARDED, AIRCRAFT DEVELOPED A SMALL VIBRATION. VIBRATION FELT IN FLOOR AND YOKE AND WOULD CHANGE WITH POWER CHANGES. ALL PARAMETERS NORMAL. WHEN LEFT ENGINE WAS SHUT DOWN AT GATE AND DECELERATED VIBRATION GOT WORSE AND AIRCRAFT ACTUALLY WOBBLED AS ENGINE SPUN DOWN.

Part: SKIN — CRACKED (RT WING) · airframe 65,673 hrs · 47,141 cycles

RT WING CRACK APPROX 3 1/2 IN LONG 12 IN O/B OF AILERON. INSTALLED PERM REPAIR PER SRM 57-01 FIG 3 SH2.

Part: CAP — UNSECURE (APU OIL) · airframe 65,489 hrs · 46,999 cycles

RETURNED TO DEPARTURE DUE TO AN ACID ODOR AND HAZE IN THE CABIN AFTER TAKEOFF. BOTH AFT LAVATORY SMOKE DETECTORS SOUNDED. MAINTENANCE FOUND THE APU OIL CAP NOT SECURE. THE APU WAS REPLACED AND WC 2120-2368 COMPLETED. THE RT ACM WAS ALSO REPLACED BECAUSE OF AN OIL LEAK. MAINTENANCE PERFORMED A DUCT BURNOUT AND REPLACED THE COALESCER BAGS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 65,433 hrs · 46,967 cycles

RIGHT MLG WW FWD DOOR FRAME CRACKED. REMOVED AND REPLACED THE DOOR FRAME IAW DWG 5930584 AND PERFORMED FIT CHECK AND PROXIMITY SENSOR CHECK IAW AMM 32-06-05. OPS CHECKED GOOD.

Part: LATCH — OUT OF ADJUST (TAILCONE) · airframe 64,137 hrs · 46,036 cycles

TAILCONE SEPARATION NOTICED ON PREFLIGHT WALK AROUND. ADJUSTED TAILCONE LOCKPIN LATCH IAW AMM 53-53-00. ALL CHECK NORMAL.

Part: FRAME — CORRODED (BS 1322) · corrosion level 2 · airframe 63,754 hrs · 45,762 cycles

CORROSION ON FRAME ON BS 1322 AND LONGERON 30. DAMAGE WAS CUT OUT IAW SRM 53-03, FIG 2A, FIG 3. HFEC WAS PERFORMED ON CUTOUT AREA, NO CRACKS WERE FOUND IAW NDT-SPM 06-10-01-001. NEW ANGLES -7-3 SECTION FILLER FRAME WERE DRILLED AND ADJUSTED IAW SRM 51-10-4. PLATES WERE FABRICATED IAW SRM 53-03, FIG 2A. REPAIR PART WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 38, 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SPM 51-30-2 AND 51-30-5.

Part: PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 65,042 hrs · 46,704 cycles

CORROSION ON T/E PANEL STA XA=400 AT LT WING. REPLACED PANEL 5912737-503.

Part: TAB — BENT (RT ELEVATOR) · airframe 63,753 hrs · 45,761 cycles

AWR BENT OTBD EDGE OF RT ELEVATOR CONTROL TAB. RT ELEVATOR CONTROL TAB WAS REPAIRED IAW SRM 55-04, PAR 3 AND CARD 2000-8149-17, JOB 000-0031.

Part: FLOOR SUPPORT — CRACKED (BS 1271-1287) · airframe 63,753 hrs · 45,761 cycles

CRACK ON FLOOR SUPPORT BETWEEN BS 1271 AND 1287 X=3. FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2, DOUBLERS REPAIRS WERE FABRICATED IAW SRM 53-01, FIG 2. DOUBLERS WERE INSTALLED IAW SRM 51-30-2, THE FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: VANE — DENTED (LT WING TE FLAP) · airframe 63,753 hrs · 45,761 cycles

SEVERAL DENTS ON REPAIR DOUBLER AT LT WING INBD FLAP INBD GUIDE VANE LOWER SURFACE. LT WING IBD FLAP INBD WAS REPAIRED IAW ERA 545145-14, REV ORIGINAL.

Part: RIB — CRACKED (LT WING) · airframe 63,753 hrs · 45,761 cycles

CRACKED RIB ON LT WING L/E BS XRS 324. STOP DRILL ON RIB IAW SRM 51-01, PAR 21, REPAIR. PARTS WERE FABRICATED IAW 57-06 B, FIG 18, REPAIR. PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5.

Part: FRAME — CRACKED (BS 1497) · airframe 63,753 hrs · 45,761 cycles

CRACKED FRAME BS 1497 LONGERONS 18L-19L IN AFT ACCESSORY COMPARTMENT. FRAME REPAIRED IAW ETI-88-16-190, REV 1 AND ER/A 545159-14, REV ORIGINAL.

Part: WEB — CRACKED (BS 1437) · airframe 63,753 hrs · 45,761 cycles

CRACK ON WEB OF BS 1437 AND LONGERON 8L AT AFT ACCESORIES COMPARTMENT. WEB WAS REPAIRED IAW ERA 519146-14MA, REV B.

Part: ANGLE — CRACKED (BS 170) · airframe 63,753 hrs · 45,761 cycles

CRACK ON ANGLE CLIP BELOW OF BEAM 1, FWD EDGE, APPROXIMATELY BS 170 AT FWD SERVICE DOOR, R1. CLIP WAS REPLACED IAW BWG 9911579, REV L AND SRM 51-30-5, SECTION SEAL WAS REMOVED AND INSTALLED IAW AMM 52-41.

Part: HOUSING — WORN (DOOR HANDLE) · airframe 63,753 hrs · 45,761 cycles

WEAR ON HOUSING OF MID CARGO COMPARTMENT DOOR HANDLE. DAMAGE HOUSING OF MID CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 51-30-2 AND 51-30.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 63,753 hrs · 45,761 cycles

CRACK ON FLOOR PANEL 541B AND 617F ALSO CRACK ON W-CHANNEL OF FLOOR PANEL 826 AT PASSENGER CABIN. FLOOR PANELS NRS 541B AND 617F WERE FABRICATED IAW AMM 53-20-01-201 W-NEW CHANNELS WERE INSTALLED ON FLOOR PANEL NR 826D REMOVED SRM 51-30-1 DRILLED SRM 51-10-4, INSTALLED DWG 9936639, REV P.

Part: DOOR FRAME — WORN (BS 1463-1474) · airframe 63,753 hrs · 45,761 cycles

WEAR ON FRAME BETWEEN CANT BS 1463 TO 1474. RT SIDE AT PASSENGER AFT ENTRANCE DOOR STAIRWAY JAMB. REPAIR PART WERE FABRICATED AND INSTALLED IAW SRM 51-70-5, FIG 2, AREA DAMAGE WAS REPAIRED IAW SRM 51-70-05, FIG 2.

Part: WEB — CRACKED (BS 628-636) · airframe 63,753 hrs · 45,761 cycles

CRACK ON WEB BETWEEN BS 636 TO 628 BETWEEN LONGERON 27 TO 28R. DAMAGE WAS REPAIRED IAW ER/A 545143-14.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 63,753 hrs · 45,761 cycles

MISSING AND DAMAGED FERRULES ON FLOOR PANEL IN PAX CABIN. REPAIRED IAW AMM 53-20-01-201.

Part: FRAME — DAMAGED (BS 1287) · airframe 63,753 hrs · 45,761 cycles

TOOL DAMAGE ON FRAME REPAIR BETWEEN LONGERON 26 LT AND 25 LT, BS 1287 AT AFT CARGO COMPARTMENT. REPAIR ANGLE WAS REPLACED, DRILLED, ADJUSTED, TRESTED AND PAINTED IAW SRM 51-10-4, 51-10-3 PAR 21 AND 14, 51-30-2, 51-30-5 AND 53-05 D, FIG 2A.

Part: ANGLE — CRACKED (BS 1463) · airframe 63,753 hrs · 45,761 cycles

CRACKED LT, RT DORSAL ANGLES BESIDE VERTICAL STAB AND BS 1463 CANT. THIS REPAIR WAS ACCOMPLISHED IAW ER/A 545157-14, REV ORIGINAL.

Part: WEB — CRACKED (BS 628-636) · airframe 63,753 hrs · 45,761 cycles

CRACK ON WEB BETWEEN BS 636 TO 628 BETWEEN LONGERON 27 TO 28R. DAMAGE WAS REPAIRED IAW ER/A 545143-14.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 63,753 hrs · 45,761 cycles

PUNCTURED, BROKEN AND DELAMINATION ON FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 25-00-00-801 P.3B.

Part: RIB — CRACKED (RT WING) · airframe 63,753 hrs · 45,761 cycles

CRACKED RIB AND RIB CLIP ON RT WING L/E BS XRS 267 APPROXIMATELY. RIB DOUBLER AND CLIP WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 63,753 hrs · 45,761 cycles

PUNCTURED, BROKEN AND DELAMINATION ON FLOOR PANEL IN PAX CABIN. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA OF ACCESS PLATE 1472C OF RT WING FUEL TANK. ACCESS PLATE NR 1472C OF RT WING FUEL TANK WAS REPLACED.

Part: CARGO TRACK — CORRODED (BS 1007-1155) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON CARGO TRACK RT SIDE FROM BS 1007 TO 1155. NEW CARGO TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: FLOOR PANEL — DAMAGED · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CRACKED AND CORRODED FLOOR PANEL. NEW FLOOR PANEL DRILLED IAW SRM 51-10-4 AND WAS INSTALLED IAW AMM 20-30-01.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 63,753 hrs · 45,761 cycles

SEVERAL SCRATCHES ON FLOOR PANEL 120A. THE FLOOR PANEL WAS REMOVED, A NEW FLOOR PANEL WAS DRILLED, TREATED AND PAINTED IAW AMM 20-30-01 AND SRM 51-10-4, 51-10-3, PAR 21 AND 14 AND INSTALLED IAW AMM 20-30-01.

Part: FRAME — CRACKED (BS 1510) · airframe 63,753 hrs · 45,761 cycles

CRACK ON FRAME BS 1510 AT 7 O`CLOCK POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911843, ITEM-5 REV AC.

Part: FRAME — CRACKED (BS 1510) · airframe 63,753 hrs · 45,761 cycles

CRACK ON FRAME BS 1510 BETWEEN 5 TO 6 O`CLOCK POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911843 ITEM-6, REV AC.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,753 hrs · 45,761 cycles

CRACKED CHANNEL ON FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131B.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 63,753 hrs · 45,761 cycles

PUNCTURED BROKEN AND DELAMINATION ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SEAT TRACK — CORRODED (BS 693-787) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT SEAT TRACK BS 787 TO 693. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1007-1220) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON CARGO TRACK LT SIDE FROM BS 1007 TO 1220 IN THE AFT CARGO COMPARTMENT. A NEW CARGO TRACK DRILLED AND ADJUSTED IAW SRM 51-10-4 WAS TREATED AND PAINTED IAW SRM 51-10-3 AND WAS INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 1497-1510) · airframe 63,753 hrs · 45,761 cycles

TWO CRACKS ON INTERCOSTAL BETWEEN CANT BS 1497 TO 1510 AT 07:00 O`CLOCK POSITION IN THE AFT ACCESSORIES COMPARTMENT. INTERCOSTAL WAS REPLACED AND CLIP IAW DM80 DWG 9917701-7-3, REV ORIGINAL AND SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 769-787) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 787 TO 769 TO BETWEEN LONGERON 28 RT TO 27 RT C2. INSTERCOSTAL WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, SRM 51-10-3 PAR 14 AND 21 DWG 9915554, REV J.

Part: CARGO TRACK — CORRODED (BS 1220-1322) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON CARGO TRACK LT SIDE FROM BS 1220 TO 1322 . NEW CARGO TRACK WAS DRILLED AND ADJUSTED IAW SRM 51-10-4 WAS TREATED AND PAINTED IAW SRM 51-10-3 AND WAS INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 63,753 hrs · 45,761 cycles

NICKS ON LOWER SKIN OF RT WING INBD FLAP ON BS XIFI=20. REPAIRED IAW SRM 57-03, FIG 8.

Part: PAN — CRACKED (BS 1155) · airframe 63,753 hrs · 45,761 cycles

CRACK ON OUTER PAN, FWD EDGE AT BS 1155 AND BEAM NR 1 IN AFT CARGO COMPARTMENT DOOR. CRACK ON OUTER PAN WAS STOPPED IAW SRM 51-01, PAR 21. HFEC INSPECTION WAS ACCOMPLISHED ON STOP HOLES, 2 E/A. NO CRACK WERE FOUND IAW SRM 51-01 PAR 21B. NEW DOUBLER WAS FABRICATED, PAINTED AND INSTALLED IAW SRM 52-03, FIG 8.

Part: BEARING — WORN (SUPPORT FITTING) · airframe 63,753 hrs · 45,761 cycles

WEAR ON BEARING AT RT MLG ACTUATOR SUPPORT FITTING. NEW BEARING AT RT MLG ACTUATOR SUPPORT FITTING WAS REPLACED IAW SOPM 20-10-7 AND ER/A 482829-14, AD REV ORIGINAL.

Part: BUSHING — WORN (HORIZONTAL STAB) · airframe 63,753 hrs · 45,761 cycles

WEAR ON BUSHINGS OF HORIZONTAL STABILIZER CENTER SECTION BOX ACCESS PANEL. REPAIR WAS PERFORMED IAW ER/A 482824-14, REV A AS PERMANENT REPAIR REF 3 REPAIR DWG ETI-88-16-174-R1.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 63,753 hrs · 45,761 cycles

SIX DENTS ON UPPER SKIN AT RT ELEVATOR CONTROL TAB. UPPER SKIN AT RT ELEVATOR CONTORL TAB WAS REPAIRED IAW DM 80, SRM 55-04, PAR 2.

Part: WEB — CRACKED (BS 1438) · airframe 63,753 hrs · 45,761 cycles

CRACK ON WEB OF BS 1438 AND LONGERON 5 RT AT AFT ACCESSORIES COMPARTMENT. CRACK WAS REPAIRED IAW ETI 88-16-156, REV 1 AND ER/A 545112-14, REV ORIGINAL.

Part: STRUCTURE — CRACKED (BS 1437) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LOWER CAP OF BS 1437 AND LONG 2 LT AT AFT ACCESORIES COMPARTMENT. LOWER CAP WAS REPAIRED IAW ETI -88-16-155, REV 1 AND ER/A 545111-14, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1438) · airframe 63,753 hrs · 45,761 cycles

TWO CRACKS ON LONGERON 3L AND BS 1438 AT AFT ACCESORIES COMPARTMENT. SECTION LONGERON STA 1438 TO STA 1447 WAS REPAIR IAW SRM 53-02, FIG 18, 51-10-3 PAR 14 AND 21, 51-30-2, 51-30-5, 51-10-2, 51-10-2A AND 51-10-4.

Part: SKIN — CRACKED (BS 1437) · airframe 63,753 hrs · 45,761 cycles

CRACK ON EXTERNAL FUSELAGE SKIN AT BS 1437 BETWEEN LONGERONS 3LT AND 4LT. CRACK WAS REMOVED AND REPAIRED IAW SRM 53-04, FIG 27.

Part: CUSP WEB — CORRODED (BS 285-288) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT CUSP WEB, BETWEEN BS 285 TO 288 AT PAX CABIN. CORROSION ON RT CUSP WEB BETWEEN BS 285 TO 288 WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: SEAT TRACK — CORRODED (BS 1016-1115) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT SEAT TRACK X -54, BS BETWEEN BS 1016-1041, 1048-1052, 1063-1070, 1079-1086, 1096-1115. DUE TO EXCESSIVE CORROSION, SEAT TRACK WAS REPLACE FROM BS 1261 IAW 80 SRM 53-05, FIG 4F AREA FROM BS 1016 TO BS 1030 WAS ATTENDED WITH CARD 377, ZONE 201.

Part: ANGLE — CRACKED (AFT CARGO DOOR) · airframe 63,753 hrs · 45,761 cycles

CRACKED TEE ANGLES AT BS 1174 AND BS 1193 BETWEEN LOWER EDGE AND BEAM NR 1 IN AFT CARGO COMPARTMENT DOOR. CRACKED TEE ANGLES AT BS 1174 AND BS 1193 BETWEEN LOWER EDGE AND BEAM NR 1 IN AFT CARGO COMPARTMENT DOOR WERE REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (BS 309) · airframe 63,753 hrs · 45,761 cycles

BLEND OUT ON FUSELAGE SKIN, BS 309 BETWEEN LONGERONS 29 RT AND 30. DAMAGE WAS DRILLED IAW SRM 53-04-2, PARAGRAPH 3. 2, A, 1, A. PLUG OF REPAIR WAS INSTALLED IAW SRM 53-04-2, 3C, 2, A, 1, A, 3.

Part: SKIN — CRACKED (RT WING) · airframe 63,753 hrs · 45,761 cycles

CRACKED RT WING FIXED L/E NEXT TO SLAT TRACK NR 8 UPPER CUTOUT. DAMAGE WAS ACCOMPLISHED IAW ERA 397957-14MA REV ORIG.

Part: LONGERON — CRACKED (BS 1438) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LONGERON 4L BS 1438. THE LONGERON WAS REPAIR IAW SRM 53-02, FIG 18, 51-10-3 PAR 14 AND 21, 51-30-2, 51-30-5, 51-10-2, 51-10-2A AND 51-10-4.

Part: SEAT TRACK — CORRODED (BS 937-1028) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT SEAT TRACK X -54 BETWEEN BS 967 - 970 , BS 984 - 986. THE SEAT TRACK, BS 935-1028 WAS REPLACED IAW SRM 53-05, FIG 4F.

Part: SKIN — CRACKED (LT WING) · airframe 63,753 hrs · 45,761 cycles

CRACKED LT WING FIXED L/E 7" OTBD FROM SLAT TRACK NR 7 CUT OUT. AREA WAS REPAIRED IAW ER/A 380953-14MA, REV A, SECTION II AS PERMANENT REPAIR.

Part: PAN — CRACKED (CABIN DOOR) · airframe 63,753 hrs · 45,761 cycles

CRACK ON EXTERNAL PAN NEXT TO LT UPPER FITTING AT AFT CABIN DOOR. CRACK ON EXTERNAL PAN WAS ACCOMPLISHED IAW SRM 52-05D, FIG 34.

Part: LONGERON — CRACKED (BS 1438) · airframe 63,753 hrs · 45,761 cycles

TWO CRACKS ON LONGERON 3L BS 1438. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-10-3, PAR 14 AND 21, 51-30-2, 51-30-5, 51-10-2, 51-10-2A AND 51-10-4.

Part: VANE — CRACKED (RT WING TE FLAP) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RT WING OTBD FLAP OTBD GUIDE VANE XV2= 301. RT WING OTBD FLAP OTBD GUIDE VANE BS XV2=301 WAS REPAIRED IAW SRM 57-03D, PAR II.

Part: FLOOR PANEL — PUNCTURED (PAX CABIN) · airframe 63,753 hrs · 45,761 cycles

PUNCTURED FLOOR PANEL 927A IN PASSENGER CABIN. DAMAGE WAS REMOVED IAW SRM 53-05. A DOUBLER WAS FABRICATED IAW SRM 53-05, PAR 3. DOUBLER INSTALLED IAW SRM 51-30-2.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,753 hrs · 45,761 cycles

WEAR ON REPAIR DOUBLER AT FWD CARGO COMPARTMENT DOOR LOWER AFT CORNER. NEW DOUBLER WAS INSTALLED IAW SRM ER/A 486624-14MA, REP ORIGINAL.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA OF ACCESS PLATE 1311C AT LT WING FUEL TANK. ACCESS PLATE WAS REPLACED.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 63,753 hrs · 45,761 cycles

DELAMINATED ON UPPER, LOWER SKIN AT RT WING GROUND SPOILER PANEL. UPPER/LOWER SKIN AT RT WING GROUND SPOILER PANEL WAS REPAIRED IAW SRM 51-70-1B.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON BARREL NUT HOLE NR 21 AND 25, AT RT HORIZONTAL SABILIZER XH=27. THE REPAIR WAS PERFORMED IAW ER/A 545118-14, REV ORIGINAL.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON BARREL NUT HOLE NR 12 AT HORIZONTAL STABILIZER CENTER BOX BS XH=6.6, LEFT SIDE. REPAIR WAS PERFORMED IAW ER/A 545119-14, REV ORIGINAL AND ETI-88-16-163-R2.

Part: CUSP WEB — CORRODED (BS 1174-1250) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON LT CUSP WEB FROM BS 1174 TO 1250 AT PASSENGER CABIN. THE CUSP WEB WAS REPLACED IAW SRM 51-10-4 AND 53-05, FIG 131A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK ACCESS PLATE NR 1303C AND 1409C. ACCESS PANELS WERE REPLACED.

Part: SUPPORT FITTING — DAMAGED (LT MLG) · airframe 63,753 hrs · 45,761 cycles

DURING BUSHING INSTALLATION, LT MLG SUPPORT FITTING WAS DAMAGED. DAMAGE WAS REMOVED IAW CARD 5740-01139-04A.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,753 hrs · 45,761 cycles

DAMAGED METALIZED COATED ON RUDDER SKIN. METALIZED COATED ON RUDDER SKIN WAS REPAIRED IAW SRA 092613-14 MA AND ACFT 0999, CARD 2000-8149-14, CREW 02 2371728.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,753 hrs · 45,761 cycles

CRACKED PREVIOUS REPAIR DOUBLER ON FLOOR PANEL NR 769A. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131B.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 63,753 hrs · 45,761 cycles

SEVERAL DENTS ON UPPER SKIN AT LT ELEVATOR GEARED TAB. SEVERAL DENTS ON UPPER SKIN AT LT ELEVATOR GERED TAB WERE REPAIRED IAW SRM 55-04, PAR 2 AND ACFT 0999, CARD 2000-8149-06, CRW 02 2322528.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 63,753 hrs · 45,761 cycles

CRACKED CHANNEL ON FLOOR PANEL. CRACKED CHANNEL REPAIRED IAW SRM 53-05 PAR 145, FIG 131B, SRM 51-10-2, SRM 51-30-2, SRM 51-10-3 PAR 14, 21.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 63,753 hrs · 45,761 cycles

PUNCTURES ON UPPER SURFACE OF RT WING OTBD FLAP MIDGUIDE VANE AT BS XV2=221 AND XV2=224.5. RT WING OTBD FLAP MID GUIDE VANE AT BS XY2=221 TO XV2=224.5 WAS REPAIRED IAW SRM 57-03D, PAR 2.

Part: SKIN — NOT REPORTED (BS 120-133) · airframe 63,753 hrs · 45,761 cycles

PREVIOUS REPAIR OF FUSELAGE SKIN BETWEEN BS 120 TO 133 AND LONGERONS 24RT TO 25RT. WAS FOUND REPAIRED SRM 53-04, FIG 2.

Part: FITTING — CRACKED (BS 1437) · airframe 63,753 hrs · 45,761 cycles

CRACKED RT LOWER DORSAL FITTING OF BS 1437 BETWEEN LONGERONS 1 TO 2 RT AT AFT ACCESSORIES COMPARTMENT. FITTING WAS REPLACED IAW SRM 51-30-5, 51-10-3 PAR 14 AND 21, ER/A 545086-14, REV ORIGINAL, AMM 20-30-01-201.

Part: ANGLE — CRACKED (BS 826) · airframe 63,753 hrs · 45,761 cycles

CRACK ON ANGLE FITTING BS 826, X=-42, Z=-10 AT CABIN PAX. REPAIR WAS ACCOMPLISHED IAW ER/A 498192-14MA, REV A.

Part: CUSP WEB — CORRODED (BS 1055-1057) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION OUT LIMITS LT CUSP WEB X=56 TO 60 BS 1055 - BS 1057 AT FLOOR STRUCTURE. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2; 53-05, FIG 131A-14.

Part: ACCESS DOOR — DAMAGED (RUDDER) · airframe 63,753 hrs · 45,761 cycles

DAMAGED COATED PAINT ON RUDDER ACCESS DOOR NR 6502G. METALLIZED WAS FOUND DAMAGED, METALLIZED WAS REMOVED. INSTALLED IAW SRM 51-70-1A --PARA 23.

Part: LONGERON SPLICE — CRACKED (BS 1437) · airframe 63,753 hrs · 45,761 cycles

CRACK ON SPLICE OF BS 1437 AND LONGERON 2RT AT AFT ACCESORIES COMPARTMENT. SPLICE WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4 AND DWG 5912141 REV. "BR".

Part: CUSP WEB — CORRODED (BS 1095-1174) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT CUSP WEB FROM BS 1095 TO 1174. RT CUSP WEB FROM BS 1095 TO BS 1174 WAS REPLACED IAW SRM 51-30-1, SRM 51-30-5, SRM 51-10-4, SRM 51-10-3 PAR 14, 21 AND SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 1287-1307) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON FLOOR SUPPORT X=0 BETWEEN BS 1287 TO BS 1307. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-30-2, 51-10-3 PAR 14, 21, 38 AND DWG 9936580, REV. BS.

Part: SEAT TRACK — CORRODED (BS 614-630) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT SEAT TRACK BS 614 AND 630 AND X=-54 AT PAX CABIN. RT SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: PAN — CRACKED (L1 DOORWAY) · airframe 63,753 hrs · 45,761 cycles

CRACK ON PAN, AFT EDGE, BETWEEN BEAM 2 AND UPPER EDGE AT FWD PASSENGER L1 DOOR. REPAIR WAS NOT NECESSARY, DUE TO FWD PASSENGER DOOR WAS REPLACED.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 63,753 hrs · 45,761 cycles

CRACK ON INTERNAL PAN AT FWD CARGO COMPARTMENT DOOR UPPER FWD CORNER. CRACK WAS STOP DRILLED. INSTALLED REPAIR IAW SRM 52-03D, FIG 8, 51-10-2, 51-30-5 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 984-1003) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON LT CUSP WEB PREVIOUS REPAIR DOUBLER BETWEEN 984-1003. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON FLOOR PANEL 160G. FLOOR PANEL AND FILLER REPLACED IAW SRM 53-01, FIG 1, SH 3, AND TRATED AND PAINTED SRM 51-10-3, PAR 21 AND 14.

Part: CUSP WEB — CORRODED (BS 522-541) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORRODED PREVIOUS REPAIR RT CUSP WEB BS 522-541, X=54-60RT AT CPAX. ON BS 522-541, X=54-60. RT CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-5, 51-30-2, 51-30-5, 51-30-1 AND DWG 9930538, REV BH.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 63,753 hrs · 45,761 cycles

DELAMINATION ON RT WING AFT BOOST PUMP SECONDARY ACCESS COVER. RT WING AFT BOOST PUMP SECONDARY ACCESS COVER WAS REPAIRED IAW ER/A 530866-14AD MA REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 1230-1240) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT CUSP WEB BS 1230 - 1240 BETWEEN X -54 AND X -60 AT CABIN PASSENGER DAMAGE WAS REMOVED AND REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131A-7 AND REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LONGERON END 7LT AND BS 1338 AT LT AFT LAVATORY AREA. LONGERON END WAS REPLACED DWG 5911422, REV B2 AND SRM 51-30-5.

Part: FLOOR SUPPORT — CRACKED (BS 1322) · airframe 63,753 hrs · 45,761 cycles

CRACK ON FLOOR SUPPORT BS 1322 X=0. THE FLOOR SUPPORT WAS REPAIRED AND STOPED IAW SRM 53-01, FIG 2 AND 51-30-2.

Part: SEAT TRACK — CORRODED (BS 227-237) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON SEAT TRACK X=-44 RT BETWEEN BS 227 TO BS 237. SEAT TRACK X=44 RT BETWEEN BS 227 TO BS 237 WAS REPAIRED IAW SRM 53-05, FIG 4A, 51-10-3, PAR 14 AND 21 AND 51-30-1.

Part: STIFFENER — CRACKED (BS 1338) · airframe 63,753 hrs · 45,761 cycles

CRACK ON STIFFENER OF BS 1338 AND PROJECTION LONG 15RT AT RT AFT LAVATORY AREA. STIFFENER ABOVE REPORTED WAS DRILLED, TREATED, PAINTED AND REPLACED IAW SRM 51-10-3, PAR 14, 21, SRM 51-30-1, SRM 51-30-5 AND DOWN 9915558, REV BA.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 63,753 hrs · 45,761 cycles

DELAMINATION ON RT WING AFT BOOST PUMP SECUNDARY ACCESS COVER. RT WING AFT BOOST PUMP SECONDARY ACCESS COVER WAS REPAIRED IAW ER/A 530866-14AD MA, REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 446-456) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION OUT OF LIMITS ON RT CUSP WEB X= 57 TO 60 BETWEEN BS 446 AND BS 456. AT FLOOR STRUCTURE. DAMAGE WAS REPAIR IAW SRM 53-05 FIG 131A-14.

Part: SKIN — CRACKED (BS 1414) · airframe 63,753 hrs · 45,761 cycles

CRACK ON INNER FUSELAGE SKIN AT BS 1414 BETWEEN LONGERONS 1 AND 2LT IN AFT ACCESSORY COMPARTMENT. CRACK WAS CUTTING OUT IAW SRM 53-04, FIG 23 AND REPAIRED IAW SRM 53-04, FIG 23. 3.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 63,753 hrs · 45,761 cycles

CRACKED INTERNAL UPPER SKIN AT VERTICAL STABILIZER L/E, RT LOWER CORNER. SKIN REPAIRED IAW ER/A 483924-14MA, REV ORIGINAL.

Part: CUSP WEB — CRACKED (BS 767-771) · airframe 63,753 hrs · 45,761 cycles

CRACKED RT CUSP WEB BETWEEN BS 767-771, X=44 TO X=54, RT ATC PASSENGER. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131-A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES OF ACCESS PLATE 1460C AT RT WING FUEL TANK. FUEL ACCESS PANEL WAS REPLACED.

Part: HOUSING — CORRODED (RUDDER YOKE) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RUDDER YOKE BEARING SUPPORT HOUSING. BY EXCESSIVE CORROSION SUPPORT HOUSING, PLATE ASSY WAS REPLACED IAW SRM 51-10-4 51-30-1 AND 51-30-2.

Part: FLOOR SUPPORT — CRACKED (BS 927) · airframe 63,753 hrs · 45,761 cycles

CRACK ON SUPPORT FITTING BS 927, X=-19, Z=-10 AT CABIN FLOOR STRUCTURE. SUPPORT FITTING WAS REPLACED, TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21; 51-10-4 , 51-30-5 AND DWG 3925812 REV A.

Part: LONGERON — CRACKED (BS 1418) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LONGERON 2L AND BS 1418 AT AFT ACCESORIES COMPARTMENT. SECTION THE LONGERON WAS REMOVED IAW SRM 51-30-5, AND INSTALLED IAW SRM 51-30-5 AND 53-14-4.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LONGERON END RT AND BS 1338 AT RT AFT LAVATORY AREA. LONGERON END ABOVE REPORTED WAS REPLACED, TREATED, DRILLED AND INSTALLED IAW SRM 51-30-5, 51-10-3 PAR 14 AND 21, SRM 51-10-4, DOWN 5911422, REV.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF RT WING FUEL TANK ACCESS PLATE 1436C. FUEL ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES OF ACCESS PLATE 1363C AT LT WING FUEL TANK. FUEL ACCESS PLATE WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 237-294) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 237 TO BS 245,BS 256 TO BS 268 AND BS 275 TO BS 294 AT CABIN FLOOR STRUCTURE. LT CUSP WEB BETWEEN BS 237 TO BS 245, BS 256 TO BS 268 AND BS 275 TO BS 294 AT CABIN FLOOR WW REPAIR IAW SRM 53-05, FIG 131A-6, 53-05 FIG 131A-14, 51-30-1, 51-30-2, 51-10-3 PAR 14, 21.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORRODED PREVIOUS REPAIR CUSP WEB BETWEEN BS 598-617, X=54-60RT AT CPAX. FABRICATED AND REPAIR PARTS WERE TREATED AND PAINTED AND REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5 AND 53-05, 51-10-3 AND 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF LT WING FUEL TANK ACCESS PLATE 1335C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT ACCESS PLATE 1470C OF RT WING FUEL TANK. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES OF ACCESS PLATE 1456C AT RT WING FUEL TANK. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKHOLES OF RT WING FUEL TANK ACCESS PLATE 1414C. 2 REPAIR BUSHINGS WERE INSTALLED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKHOLES OF RT WING FUEL TANK ACCESS PLATE 1410C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES OF ACCESS PLATE 1357C. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA OF ACCESS PLATE 1377C AT LT WING FUEL TANK. FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES AND SETTLEMENTAREA OF ACCESS PLATE 1454C AT RT WING FUEL TANK. FUEL ACCESS PLATE WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 226) · airframe 63,753 hrs · 45,761 cycles

CRACKED RT CUSP WEB BS 226, X=54 TO 60 RT AT CPAX. RT CUSP WEB, BS 226 X=54 TO X=60 RT AT CPAX WAS REPLACED DUE EXCESSIVE DAMAGE IAW SRM 51-10-4, 51-30-2 AND DWG 9930538.

Part: SKIN — CRACKED (LT WING) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LT WING FIXED L/E LOWER SKIN AT BS XOS=254. REPAIR WAS ACCOMPLISHED IAW ETI-88-16-154, REV ORIGINAL AND ER/A 543215-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT ACCESS PLATE 1466C OF RT WING. ACCESS PLATE WAS REPLACED.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 63,753 hrs · 45,761 cycles

TWO DENTS ON UPPER SKIN OF RT ELEVATOR ANTI-FLOAT TAB. SKIN WAS REPAIRED IAW SRM 55-04, FIG 1.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 63,753 hrs · 45,761 cycles

THREE DENTS ON UPPER SKIN AT LT ELEVATOR CONTROL TAB. SKIN WAS REPAIRED IAW SRM 55-04, FIG 1.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LONGERON 16 LT AND BS 1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-14-4 AND FIG 4; 51-30-2; 51-30-5.

Part: CUSP WEB — CORRODED (BS 607-649) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON LT CUSP WEB BS 607 - 612 AND 647 - 649 BETWEEN BS X=54 AND X=60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, SRM 51-30-5, SRM 51-30-1, SRM 51-30-2, SRM 51-30-1, SRM 51-10-3, PAR 14, 21, 38.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LONGERON 16 RT AND BS 1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-14-4, FIG 4; 51-30-2; 51-30-5.

Part: ANGLE — CRACKED (DOOR FRAME) · airframe 63,753 hrs · 45,761 cycles

CRACKED ANGLE BEHIND DOOR STOP FITTING NR 12 AT RT FWD OVERWING EMERGENCY EXIT DOOR. ANGLE CLIP WAS REPLACED IAW SRM 51-30-2 AND DWG 9957735, REV G.

Part: CUSP WEB — CORRODED (BS 674-693) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORRODED PREVIOUS REPAIR CUSP WEB BETWEEN BS 674-693, X=54-60, RT AT CPAX. PREVIOUS REPAIR ON CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-21 AND 51-10-3 PAR 14 AND 21 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 1063-1075) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 1063 TO 1075 AT PAX CABIN. CORROSION ON RT CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: FRAME — CRACKED (BS 1322) · airframe 63,753 hrs · 45,761 cycles

CRACK ON FRAME OF BS 1322 AND LONGERON 17R. FRAME WAS REPAIRED IAW ER/A 493697-14MA, REV B.

Part: BEARING — CORRODED (AILERON) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

RUSTED BEARING OF AILERON DAMPER LINK, OTBD POSITION, BS XA=404 APPROXIMATELY AT RT WING REAR SPAR. BEARING AT AILERON DAMPER LINK OTBD RT WING REAR SPAR WAS REPLACED IAW CMM 20-10-7.

Part: SPAR — NOT REPORTED (LT WING) · airframe 63,753 hrs · 45,761 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, 7 DIFFERENT FASTENERS OF PSE, ON LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT LT WING. THESE NRC IS ATTENDED WITH ER/A NR 545093-14AD, REV ORIGINAL.

Part: SEAT TRACK — CORRODED (BS 966-967) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON LT SEAT TRACK FROM BS 966 TO BS 967 AND X=-54 AT PAX CABIN. DAMAGE AT LT SEAT TRACK WAS REMOVED IAW SRM 53-05, FIG 4A. NEW PLUG WAS ADJUSTED IAW SRM 53-05 PAR 4A. PLUG AND REWORKED AREA WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21.

Part: SUPPORT FITTING — CORRODED (RT MLG) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON BUSHING BORE AT RT MLG ACTUATOR SUPPORT FITTING. DAMAGE ON BORE WAS REMOVED WITH FINAL DIMENTIONS AFTER REWORK: ID=2.406", THEREFORE WITHIN LIMITS IAW DWG SR09570087, REV B, NOTE 11.

Part: BUSHING — DAMAGED (LT ELEVATOR) · airframe 63,753 hrs · 45,761 cycles

SCRATCHES ON LOWER BUSHINGS XF=49 ON ATTACH POINT LT ELEVATOR. BUSHINGS OF BS XF=49 ON ATTACH POINT LT ELEVATORS WERE REPLACED IAW CMM 24-30-1.

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON BUSHING BORE AT LT MLG ACTUATOR SUPPORT FITTING. DAMAGE ON BORE WAS REMOVED WITH FINAL DIMENSIONS AFTER REWORK: ID=2.315", THEREFORE WITHIN LIMITS IAW DWG SR09570087, REV B, NOTE 11.

Part: SPAR — NOT REPORTED (RT WING) · airframe 63,753 hrs · 45,761 cycles

DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND, 7 DIFFERENT FASTENERS OF PSE, ON LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT RT WING. THESE NRC IS ATTENDED WITH ER/A NR 545093-14AD, REV ORIGINAL. WILL BE MONITORED WITH LOG PAGE NR 2427428.

Part: CUSP WEB — CORRODED (BS 885) · airframe 63,753 hrs · 45,761 cycles

CRACK ON LT CUSP WEB, BS 885, X=53, LOWER SURFACE, AT PASSENGER CABIN CRACKED ON LT CUSP WEB BS 85, X=53 WAS REPAIRED IAW SRM 53-05, FIG 131A-1 AND 51-30-2, 51-30-5, 51-10-3 PAR 14, 21, 38.

Part: WEB — CORRODED (BS 210-218) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORRODED DIAPHRAGM BETWEEN BS 210 TO 218 X=54 TO 60 RT AT CPAX. DIAPHRAGM BETWEEN BS 210 TO 218 X=54 TO 60 RT WAS REPAIRED IAW SRM 51-70-4, FIG 2, SRM 51-30-2, SRM 51-30-5, SRM 51-30-8, SRM 51-10-3, PAR 14, 21, 38.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION AND WEAR ON BORES OF LT WING SLAT PANEL NR 2, RIBS BS XOS=196, XOS=240 AND XOS=286. RIBS BORES WERE REPAIRED WITH NEXT FINAL DIMENTIONS: XOS=196, 4 HOLES: 0.938" XOS=240, 2 HOLES: 0.940" XOS=286, 2 HOLES:1.123" AND REPAIR BUSHINGS WERE FABRICATED AND INSTALLED SO THE FINAL DIMENTIONS ARE WITHIN LIMITS OF REPAIR IAW SRM 57-02, PAR 9.

Part: CUSP WEB — CORRODED (BS 1003-1022) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORRODED RT CUSP WEB NEAR TO PREVIOUS REPAIR BETWEEN BS 1003 TO 1022, X=54-60 RT AT CPAX. RT CUSP WEB WAS REPLACED IAW SRM 51-30-2, SRM 53-05, FIG 131A, SRM 51-10-3 PAR 14, 21, 38.

Part: SEAT TRACK — CORRODED (BS 577-672) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON LT SEAT TRACK BS 577 TO 578 AND 671 TO 672 AND X=22 AT PAX CABIN. DAMAGED AREAS ON LT SEAT TRACK BS 577 TO 578 AND 671 TO 672 AND X=22 WERE REPAIRED IAW SRM 53-05, FIG 4A.

Part: WEB — PUNCTURED (BS 162) · airframe 63,753 hrs · 45,761 cycles

PUNCTURE ON WEB, BS 162 AND X=6 AT E/E COMPARTMENT. REMOVED DAMAGE ON WEB AND AREA WAS TREATED AND PAINTED, PLUG WAS INSTALLED IAW SRM 53-01; 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 512-522) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON LT CUSP WEB X=60 TO X=54 ON LOWER AND UPPER SURFACE AT BS 512 TO 522. PARTS FABRICATED AREA WAS TREATED AND PAINTED INSTALLED PARTS REPAIR, ANGLE AND FITTING IAW SRM 51-30-2, 51-30-1, 51-30-5, 51-10-3, PAR 14 AND 21; 53-05, FIG 131A-14.

Part: PAN — CRACKED (BS 598) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN, AFT UPPER CORNER, BS 598, 731, 1041, 1060 AND 1079 AT CABIN PAX RT SIDE. WINDOWS RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 487747-14MA, REV A.

Part: WEB — CRACKED (BS 180-190) · airframe 63,753 hrs · 45,761 cycles

CRACKED WEB BTW X=54 TO X=44 BS 180 - 190. WEB WAS REPAIRED IAW SRM 53-01, FIG 4, SHEET 4 AND 51-30-2.

Part: WEB — CRACKED (BS 203-213) · airframe 63,753 hrs · 45,761 cycles

CRACKED WEB BETWEEN X=54 TO X=44, BS 203 TO BS 213 AT FLOOR STRUCTURE CABIN. WEB BETWEEN X=54 TO X=44, SM 203 TO 213 AT FLOOR STRUCTURE WAS REPAIRED IAW SRM 53-01, FIG 4, SHEET 4 AND 51-30-8, PAR 11.

Part: CUSP WEB — CORRODED (BS 731-739) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORRODED PREVIOUS REPAIR CUSP WEB BETWEEN BS 731-739, X=544-60 RT. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A, 51-10-3, PAR 14, 21 AND 38.

Part: CUSP WEB — CORRODED (BS 659-670) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON BRACKET AT LT CUSP WEB BS 670 AND REPAIR DOUBLER BS 659 BETWEEN BS X=54 AND X=60 AT CAB PAX. CORROSION ON BRACKET AT LT CUSP WEB WAS REMOVED, MEASURED WITH ORIGINAL THICKNESS 0.032" AND REMAINING THICKNESS 0.030". THEREFORE IT'S WITHIN OF LIMITS, TREATED AND PAINTED AND REPAIR DOUBLER WAS REPLACED IAW SRM 51-10-3 PAR 14, 21, 26, 38 SRM 51-30-2, SRM 51-30-5, PAR 7, 8, SRM 53-05, FIG 131A-13 AND ER/A 511165-14MA, REV C. (LP2438761)

Part: CUSP WEB — CORRODED (BS 678-680) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORROSION ON REPAIR DOUBLER OF LT CUSP WEB, BS 678 TO BS 680 AND BS X=54 AND X=690 AT CAB PASSENGER REPAIR DOUBLER OF LT CUSP WEB BS 678 TO BS 680, X=54 TO X=60 WAS REPLACED IAW SRM 53-05, FIG 131A-5.

Part: CUSP WEB — CORRODED (BS 712-720) · corrosion level 2 · airframe 63,753 hrs · 45,761 cycles

CORRODED PREVIOUS REPAIR CUSP WEB BETWEEN BS 712-720 X=54-60 RT AT CPAX. DOUBLER WAS REPLACED IAW SRM 51-30-2, 53-05, 51-10-3, PAR 14, 21 AND 38.

Part: PAN — CRACKED (BS 1231-1250) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN, AFT UPPER CORNER, BS 1231 AND BS 1250. RING PAN REMOVED AND REPAIRED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 788-1136) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN, AFT LOWER CORNER BS 788, BS 826 AND BS 1136 AT CABIN PASSENGER RT SIDE. DAMAGE WAS REMOVED I.AW. SRM 53-05, FIG 122 AND ER/A 487747-14 MA, REV A.

Part: PAN — CRACKED (BS 598-984) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN, FWD UPPER CORNER BS 598, BS 807 AND BS 984 AT CABIN PAX LT SIDE. RING PAN REMOVED AND REPAIRED IAW SRM 53-05 FIG12.

Part: PAN — CRACKED (BS 294-1231) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN (AFT LOWER CORNER) BS 294, BS541 AND BS 1231. RING PANS WERE REMOVED AND REPAIRED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 1022-1212) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN, FWD LOWER CORNER, BS 1022, BS 1041 AND BS 1212 AT CABIN PAX LT SIDE. CRACK ON RING PANS WERE REMOVED AND REPAIRED IAW SRM 53-05 FIG 122.

Part: PAN — CRACKED (BS 351-886) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN, FWD UPPER CORNER, BS 351 AND BS 88. RING PAN WERE REMOVED AND REPAIRED IAW IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 484-1193) · airframe 63,753 hrs · 45,761 cycles

CRACK ON RING PAN, FWD LOWER CORNER, BS 484-1193 AT CABIN PAX RT SIDE. CRACK ON RING PANS WERE REMOVED AND REPAIRED IAW SRM 53-05, FIG 122.

Part: VANE — WORN (RT WING TE FLAP) · airframe 63,753 hrs · 45,761 cycles

WEAR ON OTBD AFT CORNER OF RT WING OTBD FLAP INBD GUIDE VAVE LOWER SURFACE BS XV1=211 CANT. OTBD AFT CORNER OF RT WING OTBD FLAP INBD GUIDE VANE LOWER SURFACE BS XVI=211 WAS REPAIRED IAW ER/A 521198-14MA, REV ORIGINAL.

Part: POTABLE WATER — LEAKING · airframe 63,501 hrs · 45,588 cycles

ON DESCENT, AT 250 KTS WITH WINGS LEVEL, THE SPOILERS WERE EXTENDED TO EXT POSITION. AFTER A FEW SECONDS, THE SPOILER HANDLE SNAPPED BACK TO THE FORWARD POSITION. WHEN PULLING THE SPOILER HANDLE BACK TO THE EXT POSITION, THE AIRCRAFT ROLLED 20 DEGREES TO THE LEFT. THE HANDLE WAS STOWED AND THE ACFT RETURNED TO LEVEL FLIGHT. THE AUTOPILOT WAS THEN DISCONNECTED. THE GROUND SPOILERS OPERATED NORMALLY ON LANDING. MAINTENANCE FOUND CHUNKS OF ICE ON VARIOUS CONTROL CABLES IN THE RT WHEEL DUE TO A POTABLE WATER LEAK. THE ICE WAS REMOVED AND THE POTABLE WATER SYSTEM WAS DEFERRED. THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 62,987 hrs · 45,236 cycles

TWO INCH VISIBLE CRACK LT SIDE VERTICAL STABILIZER SKIN, BELOW ACCESS PANEL 6301A. NR 001-0283:5530-2595/003 00161. RECEIVED AND C/W WITH ERA 541996-14, REV ORIGINAL PERMANENT REPAIR. ALL REPAIR INSTRUCTIONS MATCH PRIS 541996-14, REV 0 THRU REV 4.

Part: SKIN — DENTED (ELEVATOR) · airframe 62,559 hrs · 44,930 cycles

A DENT WAS FOUND SEVEN INCHES FWD OF ELEVATOR ACCESS DOOR. REPAIRED IAW SRM 53-04-01-5B.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,604 hrs · 44,294 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE AFT CATWALK OVERHEAD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE OPS CHECK WAS GOOD.

Part: PIN — UNSECURE (L1 DOOR SLIDE) · airframe 60,693 hrs · 43,673 cycles

MAINTENANCE FOUND L1 DOOR SLIDE PARACHUTE PIN WILL NOT ENGAGE. MAINTENANCE REPLACED L1 MAIN ENTRY DOOR SLIDE ASSY IAW AMM 25-62 AND WORK CARD 2561-4964.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,650 hrs · 42,953 cycles

DURING CHECK, MAINTENANCE FOUND THE LT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHT WAS OPERATIONAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,033 hrs · 42,543 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE R & R THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIVE STATE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,927 hrs · 42,470 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 31 AND AFT IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 58,731 hrs · 42,342 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT ROW 15 WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BULB — SHORTED (EMERGENCY LIGHT) · airframe 58,510 hrs · 42,198 cycles

CABIN EMERGENCY LIGHT INOPERATIVE FROM SEAT ROW 31 ED TO THE REAR OF THE CABIN. FOUND BULB SHORTED. REPLACED BULB. OPS TESTED GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 58,090 hrs · 41,945 cycles

DURING SERVICE CHECK, NOTED THE EMERGENCY LIGHTS INOPERATIVE FROM ROW 31DE-38DE. FUSES WERE REPLACED IN THE POWER SUPPLY AT SEAT ROW 37 IAW AMM 33-53 AND OPS CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,395 hrs · 41,492 cycles

DURING LINE CHECK, MX FOUND THAT BOTH OF THE OVERWING EMERGENCY EXIT SIGNS IN THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,143 hrs · 40,626 cycles

DURING LINE CHECK, MX FOUND THAT BOTH OF THE OVERWING EMERGENCY EXIT SIGNS AND THE CEILING EEP LIGHTS FORWARD AND AFT OF THE CEILING SLIDE COMPARTMENT WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,428 hrs · 39,476 cycles

DURING SERVICE CHECK, FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE ROWS 31-36. MAINTENANCE REMOVED AND REPLACED FUSE ON BATTERY PACK B5-212. OPS CHECKED GOOD.

Part: BEAM — CORRODED (BS 1155-1212) · airframe 53,988 hrs · 39,206 cycles

DURING PSV-Q CHECK, CORROSION WAS FOUND ON THE AFT CARGO BEAM AT BS 1155-1212 AND LONGERON 28R. CORROSION WAS OUT OF LIMITS PER SRM 53-05. BEAM WAS REPLACED.

Part: SKIN — CRACKED (BS 1418 S2R) · airframe 53,988 hrs · 39,206 cycles

DURING CURRENT PSV CHECK, A CRACK TO THE FUSELAGE SKIN WAS FOUND AT STA 1418, S-2R. THE CRACK IS EMANATING FROM THE UPPER MOST FASTENER HOLE COMMON TO SHEAR TIE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,988 hrs · 39,206 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND RIGHT/LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LIGHT BATTERIES OPERATION CHECKED NORMAL. OKAY FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,660 hrs · 38,398 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE AFT GALLEY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 49,135 hrs · 36,074 cycles

CORROSION FWD CARGO DOOR JAMB INTERNAL AND EXTERNAL BEAM. BT W Y=370 TO 427. SPLICE REPAIR ACCOMPLISHED IAW SRM 53-05D FIG 804D. (DLM88101523)

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 49,135 hrs · 36,074 cycles

C1 DOOR 2EA CRACKS BEHIND STOPS NBR02 AND NB03. DOUBLER REPAIRS INTSTALLED IAW SRM52-05D FIG 50. (DLM88101524)

Part: SKIN — DELAMINATED (GROUND SPOILER) · airframe 49,135 hrs · 36,074 cycles

LT GROUND SPOILER T/E XW=47 TO 50 DELAMINATED. GROUND SPOILER T/E REPAIRED IAW SRM 51-70-1B.

Part: SUPPORT FITTING — DAMAGED (RT MLG) · airframe 49,135 hrs · 36,074 cycles

RT MLG SUPPORT FITTING BUSHING BORE OUT OF LIMITS EA 09-093855-3AD. SUPPORT FITTING WAS REAMED AND BUSHINGS INSTALLED IAW EA 09-093855-03AD.

Part: TAB — DAMAGED (RT ELEVATOR) · airframe 49,135 hrs · 36,074 cycles

RT ELVATOR CONTROL TAB LIGHTENING STRIKE REPAIR ACCOMPLISHED IAW SRM 55-04 PAR 3A.

Part: BUSHING — CORRODED (LT MLG SUPPORT) · airframe 49,135 hrs · 36,074 cycles

PITTING CORROSION ON LT GEAR SUPPORT FITTING BUSHING. LT MLG SUPPORT FITTING BUSHING BORE WAS MACHINED TO REMOVE CORROSION IAW EA 09-093855-03 AD 0109.

Part: TAB — DAMAGED (RUDDER) · airframe 49,135 hrs · 36,074 cycles

DAMAGED METALLIZED COAT ON RUDDER CONTROL TAB. METALLIZED COAT ON RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1AD PARA 23. (DLM88101533)

Part: SKIN — CORRODED (BS 1312-1322) · corrosion level 2 · airframe 49,135 hrs · 36,074 cycles

CORROSION BTW DOUBLER AND FUSELAGE SKIN ON LAV SERVICE PNL STAY=1312 TO Y=1322 BTW LONGS 19LH AND 22LH. REPAIR WAS ACCOMPLISHED IAW ERA 482821-14 REV ORIG. (DLM88101535)

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 49,030 hrs · 36,000 cycles

DURING MAINTENANCE CHECK FOUND EMERGENCY TRACK LIGHT AT 35D INOP. REPLACED SEAT WIRE HARNESS AT SEAT 35D. OPERATIONAL CHECK OF LIGHTS IS NOW GOOD.

Part: HINGE — CORRODED (VERTICAL STAB) · airframe 46,950 hrs · 34,718 cycles

VERTICAL FIN LEFT AND RIGHT O/B PIVOT FITTING PLATES CORRODED. FOUND DURING REMOVAL OF HORIZONTAL FOR UPPER SKIN REPLACEMENT DUE TO TIME LIMITED REPAIR OF CRACK. REPLACED BOTH OUTBOARD PLATE SETS PER ERA 475781-14. THESE PLATES WERE SUBJECT TO SB MD80-55-054, AD99-07-14 EO 09-073278-12AD. THE TERMINATING ACTION WAS COMPLIED WITH IN JULY OF 2004, HOWEVER THE CURRENT DAMAGE MATCHES THAT SOUGHT BY THE ORIGINAL MANDATED INSPECTION.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 46,950 hrs · 34,718 cycles

LT UPPER AFT SPAR CAP CRACKED. SPLICE NEW SECTION OF LT UPPER SPAR CAP PER EA 09-460214-12 REV D ME15

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 46,950 hrs · 34,718 cycles

06/18/09 FOUND CRACK IN RT HORIZONTAL STABILIZER REAR SPAR UPPER CAP. COLD WORKED AND BUSHED HORIZONTAL STABILIZER REAR SPAR UPPER CAP.

Part: SPAR CAP — UNKNOWN (HORIZONTAL STAB) · airframe 46,950 hrs · 34,718 cycles

HORIZ STABILIZER REAR SPAR UPPER CAP AFT SKIN REPAIR IAW 09-460214-12, C/W 09-460214-12, ME15 CAP SPLICE IAW DWG SR09550027.

Part: ENGINE — SEIZED (NR 1) · airframe 38,709 hrs · 29,455 cycles

LT ENG OIL PRESS BEGAN FLASHING ON TAKEOFF OIL PRESS REACHED 58 PSI. THE OIL PRESS DROPPED BELOW 55 PSI AT APPROX 5000FT. INDICATIONS NORMAL AFTER THAT. REPLACED OIL PRESSURE TRANSMITTER, NO HELP ADJUSTED PRESSURE REGULATOR TO LOW END AT IDLE. AT T/O POWER PRESSURE READS 5 AND FLASHING. REPLACED OIL PRESS RELIEF VLV PER MM. WHILE RUNNING ENG FAILED. REPLACED ENG PER ROUTINE CARD DECK 9T102.

Part: TAIL CONE — UNSECURE · airframe 32,227 hrs · 24,881 cycles

OPS REPORTED TAIL CONE HANGING FROM A/C. CONTRACT MTC FOUND TAIL CONE PARTIALLY DEPLOYED. ONE PIN STILL ENGAGED. SLIDE DID NOT DEPLOY AND WAS DISCONNECTED. TAIL CONE REMOVED AND REINSTALLED.

Part: WIRE — DAMAGED (ROW 35) · airframe 24,428 hrs · 19,254 cycles

EMERGENCY EXIT FLOOR LIGHT AT SEAT 35 FOUND INOP DURING L/O CHECK. REPAIRED WIRING UNDERNEATH SEAT ROW 35 DEF, OPS CK NORMAL.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 24,214 hrs · 19,094 cycles

AFT TAIL CONE EMERGENCY SLIDE LOW PRESSURE. REPLACED SLIDE.

Part: COALESCER — CONTAMINATEDN (CABIN)

BOTH AFT SMOKE DETECTORS ACTIVATED AFTER TAKEOFF FOR 2-3 MINUTES. LIGHT SMOKE PRESENT BRIEFLY. REPLACED COALESCER BAGS.

Part: LIGHT — INOP (ROW 12)

ON L/O CHECK, FOUND EMERGENCY LIGHTS INOP ROW 12 AND FWD. REPLACED POWER SUPPLY.

Part: SKIN — GOUGED (BS 1323)

FUSELAGE SKIN JUST AFT OF THE LAV SERVICE PANEL WAS FOUND WITH A GOUGE. REPAIRED PER ERA 332361-14.

Part: SKIN — GOUGED (BS 398)

FUSELAGE SKIN FOUND WITH DAMAGE THAT WAS BLENDED OUT AT THE CURRENT VISIT. BLEND WAS TOO DEEP REQUIRING SKIN CUTOUT. REPAIRED PER ERA 332358-14.

Part: SKIN — DENTED (BS 237)

FUSELAGE SKIN CUTOUT TO REMOVE DENT AT FS 237 AND 243, BETWEEN L18L AND L20L. REPAIRED PER ERA 332349-14.

Part: FRAME — CRACKED (BS 1418)

DURING RTN INSPECTION, MTC FOUND A CRACK AT L2R ON THE FS 1418 FRAME; IN TYPICAL LOCATION. REPAIRED PER ERA 332346-14.

Part: RIB — DAMAGED (TE MIDFLAP)

DURING CONDITION ACCEPT INSPECTION OF FLAP-A TEMP TYPE REPAIR WAS FOUND ON I/B AFT CLOSEOUT RIB, LOWER AFT CORNER. THE RIB WAS REPAIRED PER MM 57-52-0, FIG 808 BY INSTALLING A DIFFERENT DOUBLER.

Part: OXY MASK — FAILED (RT COCKPIT)

FIRST OFFICER'S O2 MASK HARNESS FAILED WHILE ATTEMPED TO USE IN FLT. REPLACED FIRST OFFICERS MASK ASSEMBLY.

Part: BRAKE — LEAKING (NR 1)

IN FLIGHT, LT HYD WENT TO 4 QTS. COMPLETED PROCEDURES, QUANTITY INCREASED. RESTORED SYSTEM ON FINAL, MAINTAINED 4 QUARTS AND GOOD PRESSURE. FOUND NR 1 BRAKE ASSY LEAKING. REPLACED SAME AND SERVICED HYDRAULICS, NO LEAKS.

Part: OIL PRESS LIGHT — ILLUMINATED (APU)

APU FAULT LIGHT WITH APU LOW OIL PRESSURE LIGHT CAME ON IN-FLIGHT. (NR 1 GEN ON PREVIOUS MCO).

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS IN AFT CABIN INOP. REPLACED BATTERY PACK.

Part: RETRACT MECH — MALFUNCTIONED (LT MLG DOOR)

ON LANDING GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR DOOR OPEN LIGHT. AIRCRAFT RETURNED ATL. CYCLED GEAR, ALL VISUAL NORMAL AND INDICATIONS NORMAL. BLED HYDRAULIC SYSTEM OF AIR, INSPECTED GEAR DOORS AND AREA, OPERATION NORMAL.

Part: ANGLE — CRACKED (LT MLG WW)

FOUND DURING C-2 LETTER CHECK, LT WHEEL WELL AFT STRIKER ANGLE CRACKED. REPAIRED PER SRM 53-05.