N966DL

Part: TERMINAL — BURNED (TRANSFORMER) · airframe 73,792 hrs · 55,210 cycles

LANDING LIGHTS, LEFT NOSE GEAR LIGHT INOPERATIVE. REPLACED NOSE LEFT TAXI LANDING LAMP IAW AMM 33-41- 01-401. NO HELP. SSM 33-41-0. FOUND TRANSFORMER T1-3 G TERMINAL BURNED. R & R NOSE GEAR LEFT LANDING LIGHT TRANSFORMER (T1-3) PER IAW WDM.

Part: ENGINE — FAILED (RIGHT) · airframe 73,548 hrs · 54,968 cycles

ATB - DUE TO RIGHT ENGINE ISSUES. FLT CREW REPORTED DURING CLIMB RIGHT OIL PRESSURE WENT TO 57 PSI AND FELT VIBRATION. FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN CABIN. PER QRH REDUCED THROTTLE FOR REMAINDER OF FLIGHT. MTC FOUND METAL ON MCD ANALYZED AS M50 AND REPLACED ENGINE. SDR REPORTED DUE TO SMOKE IN THE CABIN.

Part: SIGN — MISSING (CABIN) · airframe 72,922 hrs · 54,451 cycles

OVERWING EMERGENCY EXIT SIGNS MISSING. MAINTENANCE REPLACED THE EXIT SIGNS COVER. AIRCRAFT IS OK FOR SERVICE. (LP #4788928)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,781 hrs · 54,336 cycles

INITIAL INSPECTION;OUT OF RANGE SELF ILLUMATING EXIT SINGS FWD ENTRANCE;UPPER L2 AND AFTER GALLEY ZONE 3 EAS. EXIT SINGS FWD ENTRANCE;UPPER L2 AND AFTER GALLEY ZONE 3 EAS WERE REMOVED PER MD-88 AMM 11-00-01-201 STEP 3. B, EXIT SINGS FWD ENTRANCE;UPPER L2 AND AFTER GALLEY ZONE 3 EAS WERE INSTALLED PED MD-88 AMM 11-00-01-201 STEP 3 C. (LP1050637)

Part: FITTING — CRACKED (SLAT TRACK) · airframe 72,781 hrs · 54,336 cycles

INITIAL INSPECTION: CRACK ON FITTING OF SLAT TRACK 9 AT SLAT. SLAT PANEL NBR 3 LH WING WAS REMOVED P/N: 5922533-503 S/N: 09677 PER MD88 AMM 27-80-01 AND NEW SLAT PANEL NBR 3 WITH P/N: 5922533-503 AND S/N: DL67 WAS INSTALLED WITH AMDS 2700-4224- LH -03 JOB#000-0004. (LP1049144)

Part: TAB — DENTED (LT ELEVATOR) · airframe 72,781 hrs · 54,336 cycles

INITIAL INSPECTION: SEVERAL DENTS ON LH ELEVATOR ANTI FLOAT TAB. LH ELEVATOR ANTI FLOAT TAB P/N: 5930497-501 S/N: AS1206032 WAS REMOVED PER MD88 AMM 27-30-14-201 AND SERVICIABLE LH ELEVATOR ANTI FLOAT TAB P/N: 5930497-501 S/N: 49886 WAS INSTALLED PER MD88 AMM 27-30-14-201 PAR. 3.B.(1) TO 3. (LP1049261)

Part: LONGERON — CRACKED (BS 180-200) · airframe 72,781 hrs · 54,336 cycles

AWR AD AMDS 5330-01204-02B CRACK ON LONGERON 2 LH STA Y=200 ALSO STA Y= 180 APROX AT CABIN PAX INTERNAL AREA. LONGERON 2 LH BTW 180 TO 200 WAS REPAIRED PER DC-9/MD80 SRM 53-02 FIG.18 AND DWG SR09530170 REV-. (LP1041476)

Part: BRACKET — CRACKED (L1 DOOR) · airframe 72,781 hrs · 54,336 cycles

INITIAL INSPECTION: CRACK ON BRACKET INTERNAL STRUCTURE THROUGH THE OPENING MECHANISM OF L1 DOOR. BRACKET ON INTERNAL STRUCTURE THROUGH THE OPENING MECHANISM OF L1 DOOR WAS REPLACED PER DC-9/MD-80 SRM 51-30-2 AND 51-30-5 AND DWG 9955763 REV. L. (LP1040115)

Part: DOUBLER — WORN (FWD CARGO BAY) · airframe 72,781 hrs · 54,336 cycles

INITIAL INSPECTION: WEAR ON LOWER FWD DOUBLER AT FWD CARGO COMPARTMENT DOOR. LOWER FWD DOUBLER AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER DC-9/MD-80 SRM 51-30-2 AND ER/A 486624-14MA REV. ORIGINAL. (LP1039055)

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 72,444 hrs · 54,055 cycles

EMERGENCY LIGHTS AFT OF L2 DOOR INOP. REPLACED FUSE IN BATTERY PACK AND BATTERIES FOR AFT OVERHEAD EMERGENCY LIGHT PER MD88 AMM 33-53. CKS GOOD. (LP5044494)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,032 hrs · 53,718 cycles

AFT OVERWING EXIT DOORS EXIT LIGHTS INOP. REPLACED BATTERY PACK B 5105 PER MD 88 AMM 33-53. INSTALLED COVER AND PANEL. CKS OK. (LP5221583)

Part: UNKNOWN — SMOKE (APU) · airframe 72,032 hrs · 53,718 cycles

AFTER SERVICING APU OIL AND RUNNING APU FOR LEAK CHECK. APU SMOKED CABIN WITH NO EXTERNAL LEAKS FROM CAP. R/R OF APU PER WORK CARD 4900-2121, LEAK / OPS NORMAL , NO LEAKS. PERFORMES AIRCONDITIONING SYSTEM OIL CONTAMINATION CLEANING. NO OIL CONTAMINATION FOUND IN THE SYSTEM PER W/C 2120-2368 TO ITEM 6. 868016. COMPLETED WORK CARD 2120-2368. AND 7100-2619. APU WAS REPLACED W/C 4900-2121. NO SMOKE ODOR PRESENT DURING FULL DUCT BURN. (LP5221584)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,754 hrs · 53,481 cycles

CEILING EMERGENCY LIGHTS ROWS 1-10 INOP. REPLACED BATTERIES IN EMERGENCY BATT PACK B5-100 PER MD88 AMM 33-51. OPS CHECK GOOD OK FOR SERVICE. (LP5221229)

Part: PIN — STIFF (TAILCONE LATCH) · airframe 71,173 hrs · 52,983 cycles

TWO LOWER TAILCONE LATCH LOCK PINS WERE STIFF AND WOULD NOT RELEASE UNDER SPRING PRESSURE. REPLACED THE LATCH PINS IAW AMM 53-53-00.

Part: TAIL CONE — OUT OF ADJUST · airframe 71,173 hrs · 52,983 cycles

TAILCONE FAILED A RELEASE CHECK, WHEN ACTIVATED VIA AFT DOOR. ADJUSTED TAILCONE IAW AMM 53-53-00.

Part: CONDUIT — CRACKED (TAILCONE RELEASE) · airframe 71,173 hrs · 52,983 cycles

LOWER TAILCONE RELEASE CABLE CONDUIT, RT SIDE WAS CRACKED THROUGH. REPLACED THE CONDUIT IAW AMM 53-53-00.

Part: RELEASE CABLE — DAMAGED (TAILCONE) · airframe 71,173 hrs · 52,983 cycles

TAILCONE RELEASE CABLE DAMAGED. REPLACE THE RELEASE CABLE IAW AMM 53-53-00.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 71,154 hrs · 52,968 cycles

SLIDE PACK FELL OUT OF THE L1 DOOR ON TAKE OFF. CREW ELECTED TO DO AN AIR TURN BACK. SECURED THE SLIDE PACK IAW AMM 25-62, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,147 hrs · 52,961 cycles

SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE IN THE TAIL SECTION. REMOVED AND REPLACED THE BATTERIES B5-28 IAW AMM 33-53.

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,878 hrs · 52,731 cycles

CEILING EMER LIGHTS INOP. R&R BATTERIES IN B5-106. OPS CK SAT.

Part: CAP — LEAKING (APU OIL FILL) · airframe 70,395 hrs · 52,332 cycles

A BURNING RUBBER ODOR OCCURRED WITH APU RUNNING DURING BOARDING. MAINTENANCE FOUND AN APU OIL LEAK FROM THE SERVICING CAP AREA INGESTED INTO THE APU INLET. THE APU OIL CAP WAS REPLACED,

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,742 hrs · 51,846 cycles

FOUND EMERGENCY LIGHTS ON CEILING INOPERATIVE AT SEAT ROW 27, 28, 29. CHANGED THE BATTERY PACKS IAW AMM 33-53. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,512 hrs · 51,685 cycles

EMERGENCY EXIT LIGHTS AT SEATS 31CD TO 36CD OUT. REMOVED AND REPLACED BATTERY CHARGER PACK AT SEAT 35CD PER MD88 AMM 33-53. FOUND SHORT IN AFT MOST STAIRWAY LIGHT. RE-SECURED LIGHT AND ALL EMERGENCY LIGHTS OPS CHECKS GOOD. (LP4014355)

Part: DOOR FRAME — CRACKED (PAX DOORWAY) · airframe 67,832 hrs · 50,330 cycles

FWD PASSENGER DOOR UPPER FWD CORNER PAN CRACKED. REMOVED AND INSTALLED NEW DOOR. LEAK CHECK GOOD PER MD88 AMM 52-10-00. (LP2959437)

Part: TEE FITTING — DAMAGED (BULKHEAD) · airframe 67,832 hrs · 50,330 cycles

AFT PRESSURE BULKHEAD TEE SPLICE, BETWEEN LONGERONS 26 AND 27L WITH ONLY 2 FASTENERS ON ONE SIDE. REPAIRED IAW ERA 556897-14, REV 0.

Part: TEE FITTING — DAMAGED (BULKHEAD) · airframe 67,832 hrs · 50,330 cycles

AFT PRESSURE BULKHEAD TEE SPLICE BETWEEN LONGERONS 26 AND 27R WITH ONLY 2 FASTENERS ON ONE SIDE. REPAIRED RIGHT APB TEE SPLICE IAW ERA 556897-14, REV 0.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 67,832 hrs · 50,330 cycles

DURING ZONE FINAL, FOUND AREA OF DELAMINATION ON THE LT FLAP VANE LOWER SURFACE. REMOVED AND REPLACED IAW AMM 27-51-03-201.

Part: SKIN — CRACKED (LT WING) · airframe 67,832 hrs · 50,330 cycles

LEFT WING UPPER SURFACE SKIN CRACKED 1.250 INCHES LENGTH. COMPLIED WITH PRI 556857-14 REV 0, REV 1, & REV 2. REPAIRED IAW ER/A 556857-14 REV ORIG.

Part: FITTING — CRACKED (HORIZONAL STAB) · airframe 67,832 hrs · 50,330 cycles

HORIZONTAL STAB, CENTER BOX FWD END, UPPER FITTING CRACKED ON RT SIDE, HSS XH 7. REPAIRED IAW DWG 5910405-401.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 67,832 hrs · 50,330 cycles

RIGHT WING INBOARD FLAP UPPER SURFACE DAMAGED. . REPAIRED IAW ERA 556877-14 REV ORIG. REMOVED AND INSTALLED LOWER SECTION WEDGE ASSY IAW AMM 57-50-00 AND REPLACED WEAR STRIP IAW CMM 27-50-01.

Part: ROD END — DAMAGED (RT ELEVATOR TAB) · airframe 67,832 hrs · 50,330 cycles

RT ELEVATOR GEAR TAB, OTBD CONTROL ROD, FWD ROD END PULLING OUT OF ROD, RIVET SHEARED AND NUT LOOSE. REPAIRED IAW AMM 27-30-04.

Part: WEB — CRACKED (AFT STAIR) · airframe 67,832 hrs · 50,330 cycles

AFT FUSELAGE VENTRAL STAIRS, LT SIDE CANTED WEB CRACKED. REPAIRED IAW ERA 557101-14, REV ORIG.

Part: CYLINDER — CORRODED (NLG STRUT) · corrosion level 2 · airframe 67,832 hrs · 50,330 cycles

SPLINES ON OUTER CYLINDER AND BOWL ARE CORRODED ON THE NLG. REMOVAL AND REPLACED THE LANDING GEAR ASSY IAW AMDS 3242-4522, AND 3221-4152.

Part: SKIN — CRACKED (LT WING TIP) · airframe 67,832 hrs · 50,330 cycles

LEFT WING TIP AFT OF LIGHT LOWER SURFACE SKIN CRACKED. REMOVED AND REPLACED LT WING TIP IAW AMM 57-20-02. (LP2951139)

Part: BULKHEAD — CRACKED (BS 1463) · airframe 67,832 hrs · 50,330 cycles

BULKHEAD BS 1463, BETWEEN LONGERONS 7 & 9R, WEB CRACKED AT CENTER LOCATION. REPAIRED IAW PRI 557035-14 REV 0.

Part: BULKHEAD — CRACKED (BS 1463) · airframe 67,832 hrs · 50,330 cycles

AFT FUSELAGE, TAIL INTERIOR, CANTED BULKHEAD BS 1463 FWD WEB CRACKED. REPAIRED IAW PRI 557035-14 REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,832 hrs · 50,330 cycles

CRACK ON FRAME AT STA 1510 AT GUIDE PIN HOLE APPROX 4:00 OCLOCK POSITION. INSTALLED DOUBLER AND FILLER PER ERA 497316-14MA REV C.

Part: SUPPORT BRACKET — CRACKED (RT SPOILER) · airframe 67,832 hrs · 50,330 cycles

RT FLT SPOILER O/B TORQUE ARM SUPPORT BRACKET CRACKED. REPAIRED BRACKET PER SRM 57-09 FIG 33 AND REMOVED AND RE-INSTALLED TORSION BAR PER AMM 27-61-06.

Part: VANE — WORN (RT WING TE FLAP) · airframe 67,832 hrs · 50,330 cycles

RIGHT AFT FLAP INBD VANE HAS A WORN UPPER SURFACE AT REPAIR. REPLACED THE VANE.

Part: WIRE — DAMAGED (TEMP SENSOR) · airframe 66,314 hrs · 49,210 cycles

THE NR 2 ENGINE OIL TEMP SLOWLY CLIMB TO THE 135 DEGREE LIMIT, FLIGHT CREW FOLLOWED QRH PROCEDURE AND OIL TEMPERATURE COOLED FOR A SHORT TIME. OIL TEMPERATURE EVENTUALLY EXCEEDED 165 DEGREES AND FLIGHT CREW SHUTDOWN THE NR 2 ENGINE AND DECLARED AN EMERGENCY. MAINTENANCE FOUND BAD WIRE IN CONNECTOR P1-182, CONNECTOR AND OIL TEMP SENSOR WERE REPLACED. C/W OIL TEMP IMMERSION THERMOCOUPLE TEST, ENGINE RUN CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 64,916 hrs · 48,245 cycles

LIGHTNING STRIKE DAMAGE. RIGHT ELEVATOR CENTER TRIM TAB T/E. REMOVED RT GEARED TAB ON AMDS CARD DECK 2730-4130, RT. PART TO BE INSTALLED & RIGGED ON SAME AMDS CARD DECK. INSTALLED RT GEARED TAB ON AMDS CARD DECK 2730-4130 RT.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 64,916 hrs · 48,245 cycles

LIGHTNING STRIKE DAMAGE FOUND T/E OF LT ELEVATOR TRIM TAB. CENTER TRIM TAB. REMOVED LT GEARED TAB ON AMDS CARD DECK 2730-8130 LT. PART TO BE INSTALLED & RIGGED ON SAME AMDS CARD DECK. INSTALLED LT GEARED TAB ON AMDS CARD DECK 2730-8130 LT.

Part: SKIN — CORRODED (BS 1302-1322) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER FROM STA Y=1302 TO 1322 AND LONGERON 22L. CORROSION WAS REMOVED AND AREA OUT LIMIT WAS REPAIRED IAW ER/A 533315-14, REV ORIGINAL.

Part: SKIN — WORN (LT MLG DOOR) · airframe 63,004 hrs · 46,886 cycles

WEAR ON LT MLG STRUT DOOR INBD SKIN ON FWD LWR EDGE AND LWR AFT EDGE. LT MLG STRUT DOOR WAS REPAIRED IAW AC 0966 CARD 2000-8149-02, JOB 000-0004 AND ETI-88-15-116, REV 1, ER/A 534333-14, REV ORIGINAL, LP 1903243 .

Part: SKIN — CRACKED (BS 209) · airframe 63,004 hrs · 46,886 cycles

CRACKED FUSELAGE SKIN ON FS Y=209 AND LONGERON 6L. SKIN WAS REPAIRED IAW ETI-88-15-112 REV 1 AND ER/A 534327-14, REV ORIGINAL. LP 1901509.

Part: LONGERON — DAMAGED (BS 1289) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LONGERON 22 LT AND BS 1289 AT AF CARGO COMPARTMENT. LONGERON WAS ROUND WITH EXCESSIVE DAMAGE WAS REPAIRED IAW SRM 53-02, FIG 18. LP 1900697.

Part: ACCESS PANEL — CORRODED (WING) · airframe 67,069 hrs · 49,792 cycles

FUEL TANK ACCESS PANEL 1472C COUNTERSINK CORRODED OUT OF LIMITS, THE ACCESS PANEL WAS REPLACED.

Part: ANGLE — CORRODED (BS 1427-1338) · airframe 67,069 hrs · 49,792 cycles

TEE ANGLE CORRODED OUT OF LIMITS BETWEEN BS 1427-1338 AT LONGERON 25L. THE TEE ANGLE WAS REPAIRED.

Part: SKIN — DAMAGED (BS 365) · airframe 63,004 hrs · 46,886 cycles

LIGHTNING DAMAGE ON FUSELAGE SKIN STA Y=365 BETWEEN LONGERON 23LT AND 22 LT. FUSELAGE SKIN WAS REPAIRED IAW 53-04-2, FIG 2, SHEET 3. LP 1897946.

Part: DOOR FRAME — CORRODED (BS 373-423) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LOWER DOOR JAMB BEAM PAN, RT LONGERON PROJECTION 28 FS Y=373 TO Y=423 . LOWER DOOR JAMB WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. NEW LOWER DOOR WAS INSTALLED IAW 51-30-2 AND 51-30-5, LP 1897718.

Part: SKIN — CORRODED (BS 368-428) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON DOUBLER REPAIR BETWEEN RT LONGERON PROJECTION 27 AND 26 FS Y=368 AND Y=428 AT DOOR JAMB C1. DOUBLERS WERE REMOVED IAW SRM 51-30-5. NEW DOUBLERS WERE INSTALLED IAW SRM 51-30-5.

Part: DOOR FRAME — CORRODED (BS 640-690) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LOWER DOOR JAMB EXISTING DOUBLER REPAIR AT RT LONGERON PROJECTION FS Y=640 TO Y=690, C2. REPAIR DOUBLER DOOR JAMB WAS REPAIRED, TREATED, PAINTED AND INSTALLED IAW SRM 53-05, FIG 123, 51-10-3, PAR 21, 14, 38, 51-30-5 AND 51-30-4.

Part: FLOORBEAM — CORRODED (BS 1319) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON FLOOR SUPPORT, FS 1319 IN AFT CARGO COMPARTMENT AFT BULKHEAD. FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2 CORROSION IN FLOOR SUPPORT WAS REMOVED IAW SRM 51-10-3, PAR 26 AND ERA/ 511165-14, MAR REV B, DOUBLER TO REPAIR WAS FABRICATED IAW SRM 53-01, FIG. 2. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30- 2 AND FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: LONGERON SPLICE — CORRODED (BS 1195-1210) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LONGERON SPLICE 28LT BETWEEN FS Y= 1195 AND Y=1210 AT AFT CARGO COMPARTMENT, C3. LONGERON SPLICE 28LT BETWEEN STA Y=1195 AND Y= 1210 WAS REPLACED IAW SRM 51-30-5 AND DWG 5936667, REV CD. LP 1896485.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT RT FUEL TANK ACCESS PANEL 1454C. RT FUEL TANK ACCESS PANEL 1454C WAS REPLACED. LP 1896715.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT RT FUEL TANK ACCESS PANEL 1470C IN REF CARD 5, ZONE 10. RT FUEL TANK ACCESS PANEL 1470C WAS REMPLACED. LP 1896585.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT RT FUEL TANK ACCESS PANEL 1478C. RT FUEL TANK ACCESS PANEL 1478C WAS REPLACED.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,004 hrs · 46,886 cycles

CRACKED LONGERON 3R, FS Y= 1437 AT AFT ACCESORIES COMPARTMENT, SM. LONGERON WAS REPAIRED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-5 53-02, FIG 18. LP 1896669.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT RT FUEL TANK ACCESS PANEL 1476C. ACCESS PANEL 1476C OF RT FUEL TANK WAS REPLACED. LP 1896741.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AT LT FUEL TANK ACCESS PANEL 1363C. CORROSION ON HOLES COUNTERSINK ACCESS PANEL 1363C WAS R & R IAW AMM 28-00-00-201. LP 1895474.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS LT FUEL TANK ACCESS PANEL 1365C. CORROSION ON HOLES COUNTERSINK ACCESS PANEL 1365C WAS R & R IAW AMM 28-00-00-201. LP 1895472.

Part: DOOR FRAME — CORRODED (BS 1209-1158) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LOWER DOOR JAMB EXISTING DOUBLER REPAIR AT RT LONGERON PROJECTION 28 BETWEEN STA Y=1209 AND 1158, C3. DOUBLER WAS REPLACED IAW SRM 51-30-5. LP 1895944.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT RT FUEL TANK ACCESS PANEL 1464C. RT FUEL TANK ACCESS PANEL 1464C WAS REPLACED. LP 1896745.

Part: DOUBLER — CRACKED (BS 427) · airframe 63,004 hrs · 46,886 cycles

CRACK OF 1.250" ON INTERNAL PRODUCTION DOUBLER FS Y=427 BETWEEN LONGERON 25-26 RT ON LOWER AFT CORNER AT FWD CARGO DOOR JAMB. PARTS WERE REMOVED IAW SRM 51-30-2, DAMAGE WAS REMOVED IAW SRM 53-05, FIG 105, WERE FABRICATED PARTS REPAIR, IAW SRM 53-05, FIG 105, WERE TREATED AND PAINTED PARTS REPAIR IAW SRM 51-10-3, PAR 21 AND 14, WERE INSTALLED REPAIR PARTS IAW SRM 53-05, FIG 105, AND WERE INSTALLED. LP 1896517.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AT RT FUEL TANK ACCESS PANEL 1456C. CORROSION ON HOLES COUNTERSINK ACCESS PANEL 1456C WAS R & R IAW AMM 28-00-00-201. LP 1895715.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,004 hrs · 46,886 cycles

CRACKED LONGERON 3L FS Y=1437 AT AFT ACCESSORIES COMPARTMENT, SM. LONGERON WAS REPARED IAW SRM 51-30-2, 51-10-4, 51- 10-3 PAR 14 AND 21, 51-30-5 53-02, FIG 18. LP 1896673.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT RT FUEL TANK ACCESS PANEL 1462C IN REF CARD 5, ZONE 10. AYP, CORROSION ON HOLES COUNTERSINK ACCESS PANEL 1462C WAS R & R IAW AMM 28-00-00-201. LP 1895956.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,004 hrs · 46,886 cycles

CRACKED LONGERON 4R STA Y= 1437 AT AFT ACCESSORIES COMPARTMENT, SM. LONGERON WAS REPARED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-5 53-02, FIG 18. LP 1896678.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION FRAME Y=1380 LWR SECTION AT AFT ACCESSORIES COMPARTMENT. FRAME TEE WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, PARS 21, 14 & 38. LP 1895919.

Part: RUB STRIP — DEBONDED (BS 731-826) · airframe 63,004 hrs · 46,886 cycles

DISBONDED FWD LT RUB STRIPS BETWEEN STA Y=731 TO Y=826 SM. RUBSTRIP DAMAGES WERE REMOVED, NEW RUBSTRIPS WERE FABRICATED, AREA WAS CLEANED. NEW RUBSTRIPS WERE TREATED AND PAINTED AND NEW RUBSTRIPS WERE BONDED IAW ER/A: 479444-14MA, REV E. LP 1894351.

Part: INTERCOSTAL — CORRODED (BS 1147-1155) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON INTERCOSTAL FROM STA Y=1147 TO Y= 1155 BETWEEN LONGERON 30-29 RT. INTERCOSTAL CLIPS AND SUPPORT WERE REMOVED IAW SRM 51-30-2 INTERCOSTAL WAS FABRICATED IAW DWG 936071 NEW INTERCOSTAL WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14 INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, CLIPS AND SUPPORT WERE INSTALLED IAW SRM 51-30-2, 51-30-5. LP 1894782.

Part: SKIN — DAMAGED (LT WING) · airframe 63,004 hrs · 46,886 cycles

ELONGATED HOLES ON UPPER, LOWER SKIN AT LT WING TIP. ELONGATED HOLES ON UPPER, LOWER SKIN REPAIR IAW EA 09-478904-14MA, SECTION 2, PAGE 2 AFT MOUNT HOLES REPAIR. LP 1893532

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON FAYING SURFACE AT RT FUEL TANK ACCESS PANEL 1409C. FUEL TANK ACCESS PANEL 1409C WAS REPLACED IAW SRM 51-22-2A, STEP 6, PAR B.

Part: CARGO TRACK — CORRODED (BS 1007-1231) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT TIE TRACK FROM BS Y=1007 TO Y= 1231 AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE CORROSION ON TIE TRACK. LT TIE TRACK WAS REPLACED IAW SRM 51-10-4 AND IPC 25-50-00.

Part: CARGO TRACK — CORRODED (BS 1214-1226) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT TIE TRACK SPLICES BOTH SIDES UPPER AND LOWER SURFACES BETWEEN BS Y= 1214 AND Y= 1226 AT AFT CARGO. CORROSION WAS REMOVED AND NEW SPLICES WERE MANUFACTURED AND INSTALLED IAW DWG 5936660, REV BV, SRM 51-10-3, PARS 21 & 14 AND 51-30-5. LP 1892903.

Part: SKIN — DAMAGED (RT WING) · airframe 63,004 hrs · 46,886 cycles

ELONGATED HOLES ON UPPER, LOWER SKIN AT RT WING TIP. ELONGATED HOLES ON UPPER, LOWER SKIN REPAIR IAW EA 09-478904-14MA SECTION 2, PAGE 2. AFT MOUNT HOLES REPAIR.

Part: CARGO TRACK — CORRODED (BS 1222-1250) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT TIE TRACK FROM BS Y= 1222 TO Y= 1250 UPPER AND LOWER SURFACES AFT CARGO BAY. DUE EXCESSIVE CORROSION ON TIE TRACK WILL REPLACED. NEW TIE TRACK WAS INSTALLED IAW SRM 51-10-4 AND DWG 5936660.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1303C. FUEL TANK ACCESS PANEL 1303C WAS REPLACED IAW SRM 51-22-2A, STEP 6, PAR B. LP 1893796

Part: SUPPORT — BROKEN (BS 1136) · airframe 63,004 hrs · 46,886 cycles

BROKEN RT SLANT SUPPORT BS 1136 AT AFT CARGO COMPARTMENT. SLANT SUPPORT WAS REPLACED IAW ER/A 413029-14MA, REV.D.

Part: ACCESS DOOR — WORN (FUSELAGE) · airframe 63,004 hrs · 46,886 cycles

WORN ELEVATOR ACCUMULATOR ACCESS DOOR AT AFT ACCESSORIES COMPARTMENT. ACCESS DOOR WAS REPLACED. LP 1891517

Part: SUPPORT — BROKEN (BS 1271) · airframe 63,004 hrs · 46,886 cycles

BROKEN LT SLANT SUPPORT BS 1271 AT AFT CARGO BAY. SLANT SUPPORT WAS REPLACED IAW DAL ER/A 413029-14MA, REV D.

Part: LONGERON — CRACKED (BS 200) · airframe 63,004 hrs · 46,886 cycles

CRACKED LONGERON 4 LT AT BS 200. LONGERON REPLACED IAW SRM 51-30-5, 53-14-1, FIG 3.

Part: DOUBLER — WORN (ELEVATOR) · airframe 63,004 hrs · 46,886 cycles

WORN INTERNAL PRODUCTION DOUBLER ON ELEVATOR. ACCUMULATOR ACCESS CUTOUT AT AFT ACCESSORIES COMPARTMENT. DOUBLER WAS REPLACED IAW SRM 51-30-2, DWG 5917686, REV AA ON ELEVATOR ACCUMULATOR ACCESS CUT OUT AT AFT ACCESSORIES COMPARTMENT.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1379C. CORROSION ON HOLES COUNTERSINK AT FUEL TANK ACCESS PANEL 1379C WAS REMOVED. THE MAX DIAMETER IS 0.532 AND FOUND 3 HOLES ADJACENT WITH 0.537, 0.536 AND 0.537. THE MAX BUSHING IAW DOOR ALLOWED ARE 2 THEREFORE ACCESS PANEL WAS REPLACED. LP 1889926

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1357C. CORROSION ON HOLES COUNTERSINK ACCES PANEL 1357C WAS REMOVED. THE MAX DIAMETER ALLOWED IS 0.532 AND FOUND 3 HOLES DAMAGED ADJACENT WITH .554, .551 AND .538. THE MAX BUSHING PER DOOR ALLOWED ARE 2, THEREFORE, ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A. LP 1889935

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE, COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1355C. CORROSION ON HOLES COUNTERSINK ACCESS PANEL 1355C WAS REMOVED. THE MAX DIAMETER ALLOWED IS 0.532 AND FOUND 3 HOLES ADJACENT WITH 0.572, 0.547 AND 0.565. THE MAX BUSHING PER DOOR ARE 2, THEREFORE, ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — CRACKED (BS 256-275) · airframe 63,004 hrs · 46,886 cycles

CRACK ON RACKS COWLING EXHAUST AT FUSELAGE SKIN BETWEEN BS Y= 256-275 AND LONGS 20 LT TO 21 LT. REPAIRED WITH WELD IAW ER /A 464964-14, REV "C". LP 1889906.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT CENTRAL FUEL TANK ACCESS PANEL 2302C IN REF CARD 5, ZONE 10. CORROSION ON HOLES COUNTERSINK AT FUEL TANK ACCESS PLATE 2302C WAS REMOVED AND WAS REPAIRED WITH BUSHING. LP 1886912.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AT LT FUEL TANK ACCESS PANEL. CORROSION ON HOLES COUNTERSINKS AT LT FUEL TANK ACCESS PANEL 1371C WAS REMOVED. THE ACCESS PANEL WAS OUT LIMITS THEN THE ACCESS PANEL WAS REPAIRED WITH BUSHINGS. LP 1886884

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1377C. CORROSION ON HOLES COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1377C WAS REMOVED THE ACCESS PANEL WAS OUT LIMIT THEN THE ACCESS PANEL WAS REPAIRED WITH BUSHINGS. LP 1886926.

Part: INTERCOSTAL — CORRODED (BS 1310) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON INTERCOSTAL STA Y=1310 BETWEEN LONGERON 27LT-28LT AT AFT CARGO COMPARTMENT. REPAIR PARTS WERE FABRICATED, DAMAGE ON INTERCOSTAL WAS REMOVED, FABRICATED REPAIR PARTS WERE TREATED AND PAINTED, REPAIR PARTS WERE INSTALLED, INTERCOSTAL WAS INSTALLED AND CIC WAS APPLIED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1367C. CORROSION ON HOLE COUNTERSINKS AT FUEL TANK ACCESS PLATE, 1367C WAS REMOVED. THE MAX DIAMETER ALLOWED IS .532 AND FOUND 3 HOLES DAMAGE ADJACENT WITH .539, .535 AND .550 AND THE FUEL TANK ACCESS PLATE WAS REPLACED. LP 1886980

Part: LONGERON — CRACKED (BS 200) · airframe 63,004 hrs · 46,886 cycles

CRACKED LONGERON 2 LT AT STA Y=200, SM. SECTION DAMAGE FROM BS Y=150 TO Y=307 WAS R & R IAW SRM 53-02, FIG 18, NEW SECTION OF LONGERON WAS ADJUSTED, DRILLED, TREATED & PAINTED IAW SRM 51-10-3, PAR 21 & 14, 51-10-1, 51-30-2 AND 51-30-5, AND 53-02, FIG 18.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON FRAME PREVIOUS REPAIR BS Y= 1309 AT AFT CARGO COMPARTMENT. REPAIR PART WITH CORROSION WAS REPLACED IAW SRM 53-03 "D" FIG 2.4. IT WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21. LP 1886319

Part: FINGER DOUBLER — CORRODED (BS 1187-1195) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

INITAL AD: CORROSION ON FINGER DOUBLER REPAIR BETWEEN STA Y=1187 TO Y= 1195 AND LONGERON 29 LT TO 30 AT AFT CARGO COMPARTMENT. DOUBLER WAS REPLACED IAW SRM 53-04-2, 51-10-3, PAR 14 AND 21, 38, 51-30-5.

Part: DOUBLER — CORRODED (BS 571) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON INNER PRODUCTION DOUBLER BS X=571 BETWEEN LONG 30-29 RT AT MID CARGO COMPARTMENT. CORROSION ON INNER PRODUCCTION DOUBLER BS Y= 571 BETWEEN LONGERON 30-29 RT WAS REMOVED AND REWORKED AREAS WAS TREATED AND PAINTED IAW SRM, 51-10-3 PAR.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1361C. PLATE 1361C WAS REMOVED. THE ACCESS PLATE WAS OUT LIMITS THEN THE ACCESS PLATE WAS REPAIRED WITH BUSHINGS IAW SRM: 51-22-2A.

Part: RIB — CRACKED (RT WING) · airframe 63,004 hrs · 46,886 cycles

CRACKED RT WING L/E RIB STA XRS 271. RIB WAS REPLACED IAW SRM 51-30-2; 51-30-5 AND DWG 9937588-4, REV G.

Part: RIB — CRACKED (LT WING) · airframe 63,004 hrs · 46,886 cycles

CRACKED RIB AND CLIP ON LT WING L/E STA XRS 430. NO CRACKS WERE FOUND ON THE CLIP. REPLACED RIB, TREATED AND PAINTED IAW SRM 51-30-2, 51-10-3 PAR 14, 21, 38.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1311C. THE FUEL TANK ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 28:00-0120 ZONE 13 IAW AMM: 28-00-00.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1373C. FUEL TANK ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120 ZONE 13 IAW AMM: 28-00-00.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 63,004 hrs · 46,886 cycles

CRACKS AND ELONGATED HOLES ON FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM-51-70-1, SRM 51-70-4, AND SRM 53-05, FIG 131B, 131C.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON COUNTERSINK AT LT FUEL ACCESS PLATE NR 1335C. FUEL TANK ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120 ZONE 13 IAW AMM: 28-00-00.

Part: CUSP WEB — CORRODED (BS 1111-1117) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN STA Y=1111 TO Y=1117, AND FROM STA Y=1122 TO Y=1129 AT CABIN FLOOR. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-7 AND 131A, FIG 13 AND REPAIR PARTS WERE INSTALLED IAW SRM 51-30-5 AND 51-30-1.

Part: CUSP WEB — CORRODED (BS 1274) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT CUSP WEB UPPER/LWR SURFACE AT STA Y=1274 BETWEEN STA X=54 TO X=60 FLOOR CABIN STRUCTURE. CUSP WEB LT AT STA Y=1274 WAS REPARED IAW SRM 53-05, FIG 131A-6.

Part: CUSP WEB — CORRODED (BS 1202-1203) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB STA Y=1171,1195, AND BETWEEN 1202- 1203 X=-54-60. RT CUSP WEB ON STA Y=1171, 1195, 1202-1203 WERE REPAIRED IAW SRM 53-05, FIG 131A-9.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT CENTRAL FUEL TANK ACCESS PANEL 2301C. THE FUEL TANK ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 5730-0655.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CPCP CORROSION ON BORE INNER AND OUTER SURFACE OF RIBS FROM STA XOS=530,580 AND 610 AT LT SLAT PANEL NR 5. CORROSION ON INNER AND OUTER SURFACE OF RIBS FROM XOS = 530 AND 610 WERE REMOVED IAW SRM 51-10-3, PAR 26 WAS ACCOMPLISHED ORIGINAL THICKNESS ON RIB AT STA=XOS = 530 IS 0.370" AND MINIMUN REMAINING THICKNESS IS 0.364" THEREFORE IT IS WITHIN LIMITS IAW SRM 57-01, FIG 1B WAS ACCOMPLISHED ORIGINAL THICKNESS ON RIB AT FROM XOS =610 IS 0.251" THEREFORE IS WITHIN LIMITS IAW SRM 57-01, FIG 1 AND REPLACED RIB AT STA XOS= 580 AND XOS = 610, DAMAGE WAS REPAIRED ON STA XOS=530 AND 610 AND MEASURED WITH HOLES FWD ID 0.811" AND AFT HOLES ID 0.812" ON STA XOS =530 AND STA XOS =610 HOLES FWD AND AFT ID 0625" THEREFORE OUT LIMITS OF BLUE PRINT HOLE DIAMETER IAW SRM 57-02, PAR 9C 1. BUSHINGS WERE FABRICATE AND INSTALLED IAW SRM 57-02, PAR 9 C2.

Part: STRUCTURE — DELAMINATED (RT WING TE FLAP) · airframe 63,004 hrs · 46,886 cycles

DELAMINATION ON REPAIR DOUBLER BEHIND UPPER RUB STRIP AT RT WING INBD FLAP OTBD GUIDE VANE. RT WING INBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW SRM 57-03D.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FREYING SURFACE AT RT FUEL TANK ACCESS PANEL 1436C. ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390 IAW AMM 28-00-00.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FREYING SURFACE AT RT FUEL TANK ACCESS PANEL 1466C. OUT OF LIMITS AND ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390 ZONE 14 IAW AMM 28-00-00.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 63,004 hrs · 46,886 cycles

DENTS ON REPAIR DOUBLER AT INBD VANE, INBD FLAP RT WING. REPAIR WAS PERFORMED IAW SRM 57-03D, P11 AND JIC CARD 2000-8149-14, 9085202, JOB 000-0016.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FREYING SURFACE AT RT FUEL TANK ACCESS PANEL 1414C. OUT OF LIMITS AND ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, ZONE 14 IAW AMM 28-00-00.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FREYING SURFACE AT RT FUEL TANK ACCESS PANEL 1460C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, ZONE 14 IAW AMM 28-00-00.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FREYING SURFACE AT RT FUEL TANK ACCESS PANEL 1410C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, ZONE 14 IAW AMM 28-00-00.

Part: SUPPORT — CRACKED (BS 1174-1193) · airframe 63,004 hrs · 46,886 cycles

CRACKED SUPPORTS ON STA Y=1193 AND Y=1174 BETWEEN LONGERON 8 LT TO 9 LT AT CABIN INTERNAL STRUCTURE. SUPPORTS ON STA Y=1193 AND Y=1174 BETWEEN LONGERON-8LT-9LT WAS ATTENDED WITH ER/A 531374-14 REV. ORIGINAL.

Part: PLATE — WORN (APU BAY) · airframe 63,004 hrs · 46,886 cycles

INITIAL-WEAR ON PLATE AT APU ENCLOSURE. PREVIOUS DOUBLER WAS REPLACED AND INSTALLED NEW REPARATION DOUBLER IAW SRM 51-30-8, 53-01, FIG 2 AND 51-30-2.

Part: BEARING — DAMAGED (RUDDER) · airframe 63,004 hrs · 46,886 cycles

DAMAGED BEARING OF RUDDER UPPER LOWER HINGE ATTACH POINT AT VERTICAL STABILIZER. BEARING OF RUDDER UPPER LOWER HINGE ATTACH POINT AT VERTICAL STABILIZER WERE REPLACED IAW 27-20-01-401, AMM.

Part: FLOOR PANEL — DELAMINATED · airframe 63,004 hrs · 46,886 cycles

DELAMINATED ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01 201.

Part: FLOOR SUPPORT — CORRODED (BS 1144-1150) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER BETWEEN STA Y= 1144-1150 X=-54-X=-60 AT PAX CABIN FLOOR STRUCTURE. REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 131A. LP1879490

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BORES OF RIB FROM STA XOS= 286 AT LT SLAT PANEL NR 2. DAMAGE ON BORES OF RIB STA XOS=286 WAS REPAIRED IAW ETI-88-15-099, REV ORIGINAL AND ER/A 533325-14, REV ORIGINAL.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BORES OF RIB FROM STA XOS= 380 AT LT SLAT PANEL NR 4. DAMAGE ON RIB STA XOS=380 WAS REPAIRED IAW ETI-88-15-098, REV ORIGINAL AND ER/A 533324-14 REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 1136-1222) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB BETWEEN STA Y=1136-1144, Y= 150-1174, Y=1193-1203, AND Y=1211-1222 X=-54-X=-60 AT CABIN FLOR STRUCTURE. CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3, PAR 14, 21, 26, 38 AREAS OUT LIMITS WILL BE ATTENDED WITH CARD 322, ZONE 201.

Part: CUSP WEB — CORRODED (BS 1060-1065) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON CUSP WEB BETWEEN STA Y=1060 TO Y=1065, X=54 TO X=60 AT CABIN FLOOR STRUCTURE. NEW DOUBLER WAS FABRICATED IAW SRM 53-05, FIG 131A-1. NEW DOUBLER WAS TREATED AND PAINTED I.AW SRM 51-10-3, PAR 21, 14. NEW DOUBLER WAS INSTALLED AND FITTING IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 964-966) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK X=54 AND STA Y=964-966 AT PAX CABIN. SEAT TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-5.

Part: CUSP WEB — BENT (BS 237-256) · airframe 63,004 hrs · 46,886 cycles

BENT LT CUSP WEB BETWEEN BS 237 - 256 AND X=54 TO X=60. CUSP WEB WAS REPAIR IAW SRM 53-05, FIG 131.

Part: DOUBLER — BENT (RT ELEVATOR) · airframe 63,004 hrs · 46,886 cycles

INITIAL AD: BENT LOWER STRAP DOUBLER OF RT ELEVATOR. STRAP WAS REMOVED, TRAP WAS FABRICATED, TREATED AND PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3, P14, 21 AND 55-20-01.

Part: CUSP WEB — CORRODED (BS 1258-1265) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB FROM STA Y=1258 TO X=1265, Y= 1290 TO Y=1307, BETWEEN X=-54 TO X=-60 AT CABIN FLOOR STRUCTURE. RT CUSP WEB STA Y=1258 TO 1265 AND 1290 TO 1307, CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A, UT, NDT SPM 04-0007, PARS FIG 3, SH 4, 2. ORIGINAL THICKNESS .040" AND REMAINING THICKNESS ON STA Y=1258 TO 1265 .033", AND ON STA Y=1290 TO 1307 .034" THEREFORE OT'S OUT OF LIMITS.

Part: SEAT TRACK — CORRODED (BS 1213-1219) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK X=54 BETWEEN BS 1213-1219 AND Y=1293 AT PAX CABIN. REMOVE DAMAGES ON SEAT TRACK, NEWS PLUGS WERE ADJUSTED, NEW PLUGS WERE INSTALLED IAW SRM 53-05, FIG 4A, SHEET 1.

Part: ANGLE — BENT (BS 237-256) · airframe 63,004 hrs · 46,886 cycles

BENT LT CUSP ANGLE BETWEEN STA Y=237 TO STA Y=256 AND X=59. CUSP ANGLE WAS REPAIRED IAW SRM 53-05, FIG 25.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BORE/INNER AND OUTER SURFACE OF RIBS FROM STA XIS=83,136 AND 186 AT SLAT PANEL LT NR 1. CORROSION ON OUTER SURFACE OF RIBS WERE REMOVED IAW SRM 51-10-3. RIBS WERE MESURED AS FOLLOWS ORIGINAL THICKNESS IS 0.320" REMAINING THICKNESS IS 0.277", THEREFORE IT'S WITHIN LIMITS IAW SRM 57-01, FIG 1. REWORKED AREA ON OUTER SURFACE WAS TREATED AND PAINTED IAW SRM 51-10-3. DAMAGE ON BORE OF RIBS WERE REMOVED AND MEASURED; STA XOS=83 HOLES AFT AND FWD ID 1.063" AND FWD INBD ID 1.062", STA XOS=136 HOLES AFT 0.938" AND HOLES FWD 0.950", XOS=186, HOLES FWD 0.938" THEREFORE WITHIN LIMIT OF MAXIMUM REWORK HOLES DIAMETER IAW SRM 57-02, PAR 9. BUSHING WERE FABRICATED AND INSTALLED IAW SRM 57-02, PAR 9 C 1, 2.

Part: CUSP WEB — CORRODED (BS 837) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT CUSP WEB BETWEEN X=54 AND 60 STA Y=837 AT PAX CABIN. REPLACED CUSP WEB STA Y= 807-845, NEW CUSP WEB DRILLED AND ADJUSTED IAW SRM 51-10-4, AND TREATED AND PAINTED SRM 51-10-3, PAR 21 AND 14 AND 51-30-5.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 63,004 hrs · 46,886 cycles

INITIAL INSPECTION DELAMINATED ON OUTER SKIN FROM OTBD FRAME AT LT OTBD FLAP. THE DAMAGE THEY ARE OUT OF LIMITS BY REPAIR IAW SRM 57-03D, PAR 11 THEREFORE WAS REPLACED.

Part: SKIN — CRACKED (BS 160) · airframe 63,004 hrs · 46,886 cycles

CRACK WAS FOUND ON FUSELAGE SKIN OF 0.187" AT UPPER FORWARD CORNER BS 160. FASTENERS WERE REMOVED DAMAGE WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 112.

Part: SEAT TRACK — CORRODED (BS 790-797) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT SEAT TRACK FROM STA Y=790 TO Y=797 AND X=-54 AT CABIN FLOOR STRUCTURE. SEAT TRACK WAS REPLACED BETWEEN STA Y=701-797 IAW SRM 51-30-1; 51-10-4 AND 51-10-3, PARS 14 & 21.

Part: DUCT — CRACKED (APU EXHAUST) · airframe 63,004 hrs · 46,886 cycles

CRACKED APU EXHAUST DUCT. APU EXHAUST DUCT WAS REPAIRED, REWELDED, IAW ER/A 473221-14MA.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BORED, INNER AND OUTER SURFACE ON RIBS FROM STA XOS=286, 332 AND 380 AT LT SLAT PANEL. DAMAGES ON RIBS STA XOS= 286; 332, 380 WERE REPAIRED IAW ER/A 533332-14, REV ORIGINAL AND ETI 88-15-104, REV 1.

Part: SUPPORT — CRACKED (BS 927) · airframe 63,004 hrs · 46,886 cycles

CRACKED FITTING SUPPORT STA Y=927, X=-44 AND Z=-10 AT FLOOR CABIN STRUCTURE. RT, SIDE. FITTING SUPPORT WAS REMOVED IAW SRM 51-30-1 AND 51-30-2. NEW FITTING WAS DRILLED IAW SRM 51-10-4. HOLES WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21-14. NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 63,004 hrs · 46,886 cycles

DELAMINATION ON LT OTBD VANE INBD FLAP BENEATH RUB STRIP INBD EDGE. DELAMINATED AREA WAS REPAIRED IAW SRM 57-03 D.

Part: CUSP WEB — CORRODED (BS 1250-1287) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE FROM STA Y=1250 TO Y=1271, STA Y=1271 TO Y=1287 BETWEEN X=54 TO X=60 AT CABIN FLOOR STRUCTURE. CORROSION WAS ATTENDED, REMOVED; MEASURED AND FOUND WITHIN LIMITS BETWEEN Y=1250-1271 BUT AT Y=1247 IT'S 0.035" AND SO OUT OF LIMITS, AND THIS WILL BE ATTENDED WITH CARD 313, ZONE 201.

Part: CUSP WEB — CORRODED (BS 897-902) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB FROM STA Y= 897 AND Y=902 BETWEEN X=-48 AND X=-60 FLOOR CABIN STRUCTURE. CORROSION WAS ATTENDED ON STA Y= 897 AND Y= 902 RT CUSP WEB IAW SRM 51-10-3 AND 53-05.

Part: SKIN — DAMAGED (BS 159) · airframe 63,004 hrs · 46,886 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN RT LONGERON 5 AND 6, STA Y=159. LIGHTHING STRIKE ON FUSELAGE SKIN WAS ATTENDED AND AFTER BLENDED WAS FOUND OUT OF LIMIT THEREFORE WAS REPAIRED WITH REPAIR DOUBLER AND DAMAGE WAS CUT OUT IAW SRM 53-04-1, PAR 6D, 3, COND 3. SRM 53-04-2, FIG 2, SH 17, SRM 51-30-2, 51-30-5.

Part: CUSP WEB — CORRODED (BS 490-503) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CABIN FLOOR CUSP WEB FROM BS 490 TO 503 BETWEEN X=-54 TO X=-60 UPPER AND LOWER SURFACE. CORROSION WAS ATTENDED IAW SRM 53-05, FIG 131A-6, 57-30-1, 57-10-3, PAR 14-21 AND 38 AND NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131 A-6.

Part: FLOOR SUPPORT — CRACKED (BS 965-984) · airframe 63,004 hrs · 46,886 cycles

CRACKED FLOOR SUPPORT AT BS 965 AND 984, X=-30 TO X=-37 AT RT CABIN FLOOR STRUCTURE. CRACKED FLOOR SUPPORTS WERE REMOVED DRILLED ADJUSTED AND INSTALLED IAW SRM 51-10-3, PAR 13, 14 AND 21, SRM 51-30-5 AND 53-14-3 FIG 12, 51-10-4.

Part: FLOOR PANEL — CRACKED (CABIN) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CRACK AND CORROSION ON FLOOR PANEL 160G AT PAX CABIN. FLOOR PANEL 160G AT PAX CABIN WAS REPLACED IAW SRM 51-10-3, PAR 21,14, SRM 51-10-4, DWG 9957828, REV AB.

Part: CUSP WEB — CORRODED (BS 875-880) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AT RT CUSP WEB BETWEEN STA Y= 875 AND Y=880 ALSO BETWEEN Y=835 AND Y=841 BETWEEN X=-48 AND X=-60. CUPS WEB BETWEEN STA Y 875-880 WAS REPAIRED IAW SRM 53-05, FIG 131A-4. BETWEEN ON Y 835-Y 841 WAS ATTENDED WITH CARD 316, ZONE 201.

Part: FITTING — CRACKED (BS 650) · airframe 63,004 hrs · 46,886 cycles

DURING AD INITIAL INSPECTION, A CRACK WAS FOUND ON UPPER INNER FITTING FROM STA Y= 650 AT MID CARGO COMPARTMENT. CRACK FITTING WAS REMOVED IAW SRM 51-30-1. NEW FITTING WAS FABRICATED, ADJUSTED AND DRILLED IAW SRM 51-10-4 NAD DWG N3926046-3. NEW FITTING WAS TREATED AND PAINTED IAW 51-10-3, PAR 14 AND 21. NEW FITTING WAS INSTALLED IAW SRM 51-30-1.

Part: TAB — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

FREE PLAY, CORROSION AND SCRATCHES ON ANTI-FLOAT TAB, GEARED TAB ATTACH POINTS AT RT ELEVATOR. HARDWARE ATTACH PAINT AN ANTI-FLOAT TAB AND GEARED TAB RT ELEVATOR WAS R & R NEW HARDWARE IAW CMM 20-27-1 AND FREEPLAY WAS CORRECTED.

Part: ANGLE — CRACKED (BS 650) · airframe 63,004 hrs · 46,886 cycles

AD INITIAL: INSPECTION: CRACK ON LOWER ANGLE FROM STA Y=650 AT MID CARGO COMPARTMENT DOOR. DAMAGE ANGLE WAS REMOVED. NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 1094-1097) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB FROM STA Y=1094 TO 1097 BETWEEN X=-54 AND X=-60 AT CABIN FLOOR STRUCTURE. DOUBLER REPAIR WAS FABRICATED AND TREATED, PAINTED IAW SRM 53-05 FIG 131A-10, SHEET 1 AND 51-10-3 PAR 14/21.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1307C. CORROSION FOUND TO BE OUT OF LIMITS. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: FITTING — CRACKED (BS 650) · airframe 63,004 hrs · 46,886 cycles

AD INITIAL INSPECTION: CRACK ON LOWER INNER FITTINGS FROM STA Y= 650 AT MID CARGO COMPARTMENT DOOR. DAMAGE FITTING WAS REMOVED IAW SRM 51-30-2 AND 51-30-1. NEW FITTING WAS DRILLED, TREATED, PAINTED AMD INSTALLED IAW SRM 51-10-4, SRM 51-10-3 PAR 14/ 21, SRM 51-30-02, NAD 51-30-01.

Part: DIAPHRAGM — DAMAGED (BS 160-196) · airframe 63,004 hrs · 46,886 cycles

ELONGATED HOLES ON DIAPHRAGM AT STA Y=160 TO Y=196, X=54 AT CABIN FLOOR STRUCTURE. DIAPHRAGM WAS REPAIRED IAW SRM 51-30-2, SRM 51-70-4, FIG 2, PAR 1, SRM 51-10-3, PAR 14, 21 SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 1035-1071) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB STA Y=1035, 1047 AND 1071 BETWEEN X=-54 AND X=-60 AT CABIN FLOOR STRUCTURE. CUPS WEB ON Y=1035, 1047 AND 1071 BETWEEN X=-54 AND X=-60 WERE REPAIRED IAW SRM 53-05, FIG 131A-7.

Part: WEB — CRACKED (BS 101) · airframe 63,004 hrs · 46,886 cycles

CRACK ON WEB STA Y=101, X=0, Z=-8 AT INTERNAL STRUCTURE BELOW FLOOR PANEL. WEB ON STA Y= 101, X=0, Z=-8 WAS REPAIRED IAW SRM 53-01, FIG. 2.

Part: CUSP WEB — CORRODED (BS 438-489) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CABIN FLOOR STRUCTURE CUSP WEB STA Y= 438-440, Y=459-461, Y= 480, Y=489 BETWEEN X=-54 TO X=-60. UPPER AND LOWER SURFACES. CUSP WEB STA Y=438-440, Y=459-461 WERE REPAIRED IAW SRM 53-05, FIG 131A-13. CUSP WEB BETWEEN Y=479-484 WAS REPAIRED IAW SRM 53-05, FIG 131A. DAMAGE AT Y=489 WILL BE ATTENDED WITH CARD 309, ZONE 201.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 63,004 hrs · 46,886 cycles

CRACKED CLIP FWD /AFT EDGE OF BEAM N.1 LOWER SIDE AT FWD SERVICE DOOR. CRACKED CLIP FWD/AFT WERE REMOVED IAW SRM 51-30-5. NEW CLIPS WERE INSTALLED IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 803-804) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CABIN FLOOR CUSP WEB STA Y=803-804 ALSO ON DOUBLER PREVIOUS REPAIR STA Y=838-845 BTW X=-54 AND X=-60. DOUBLER PREVIOUS WAS REMOVED AND NEW DOUBLER, RIG DOUBLER, FILLER WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW FIG 131A-2, 51-10-3 PAR. 14, 21, 51-30-5.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 63,004 hrs · 46,886 cycles

CRACKED INNER PAN FWD EDGE BELOW TO LOWER SECTION HINGE AT FWD SERVICE DOOR R1. CRACKED INNER PAN FWD WAS REPAIRED IAW SRM 52-03, FIG 3.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 63,004 hrs · 46,886 cycles

CRACKED BEAM N.1 FWD EDGE AT FWD SERVICE DOOR (R1). CRACKED BEAM N.1 FWD WAS REMOVED IAW SRM 51-30-2, 51-30-4 AND 51-30-5, NEW BEAM WAS INSTALLED IAW SRM 51-30-2, 51-30-4 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 769-788) · airframe 63,004 hrs · 46,886 cycles

CRACKED INTERCOSTAL AT STA Y=769 TO Y=788, X=0 AT CABIN FLOOR STRUCTURE. INTERCOSTAL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. NEW INTERCOSTAL WAS DRILLED IAW SRM 51-10-4. NEW INTERCOSTAL WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1035-1103) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB BETWEEN STA Y=1035-1060, Y= 1071-1083, 1094-1103 X=-54 X=-60 AT CABIN FLOOR STRUCTURE. CORROSION ON RT CUSP WEB STA Y=1036-1060, Y=1071-1083 AND Y=1094-1103 WAS ATTENDED IAW DC-9/MD80 SRM 51-10-3 PAR. 14 AND 21 AND ER/A 511165-14 MA REV B. STA Y= 1035, Y=1047, Y=1071 AND Y=1094 TO Y=1097 WILL BE ATTENDED WITH CARDS NR 304 AND 303.

Part: RIB — DAMAGED (RT WING) · airframe 63,004 hrs · 46,886 cycles

DURING MAINTENANCE ACTIVITIES. DAMAGE BORES ON RIBS STA XOS 286, 332 AND 380 AT RT SLAT PANEL NR 3. DAMAGE ON RIB STA XOS=332 WAS REWORKED AND MEASURED WITH ID 0.938, 4 HOLES, THEREFORE LIMITS OF MAXIMUM REWOK HOLE DIAMETER IAW SRM 57-02, PAR 9 C (1). BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 57-02, PAR. 9 C, 1, 2. DAMAGE ON RIB`S STA XOS= 286, 380 WERE REPAIRED IAW AND ER/A 533331-14 REV ORIGINAL.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

INITIAL CORROSION AFT BORE ON RIBS STA XOS 429 AT SLAT PANEL NR 4 RT WING. DAMAGE ON AFT BORE WAS REPAIRED IAW AND ER/A 533326-14 REV, ORIGINAL.

Part: CUSP WEB — CORRODED (BS 785-905) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CABIN FLOOR CUSP WEB FROM STA Y=785 TO Y= 905 BETWEEN X=-48 AND X= -60 UPPER ANDLOWER SURFACES AND DOUBLER REPAIR. CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 14, 21, 26. STA Y=897-902 WAS FOUND OUT OF LIMITS AND WILL BE REPAIRED WITH NRC 314 ZONE 201 AND DOUBLER WITH CORROSION WILL BE REPLACED WITH NRC 315, ZONE 201.

Part: ANGLE — CRACKED (BS 1437) · airframe 63,004 hrs · 46,886 cycles

INITIAL CRACKED FRAME CLIPS STA Y=1437 BETWEEN LONGERONS 2L-3L, 1-2R AT AFT ACCESSORIES COMPARTMENT. CLIPS WERE REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-3 PAR 14 AND 21 AND DWG 9911840-112 AND 116 REV DC.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,004 hrs · 46,886 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

INITIAL CORROSION FWD BORE ON RIB STA XOS 380 AT SLAT PANEL NR 4 RT WING. DAMAGE ON RIB STA XOS= 380 WAS REMOVED AND MEASURED, WITH ID 1.1265 ON FWD HOLE, THEREFORE OUT LIMIT OF MAXIMUM REWORK HOLE DIAMETER, THEREFORE WAS REPAIRED WITH AND ER/A 533326-14, REV.

Part: CUSP WEB — CORRODED (BS 503-580) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CABIN FLOOR CUSP WEB STA Y=503, Y=553 AND Y=580 BETWEEN X=-54 AND X=-60. CABIN FLOOR CUSP WEB STA Y=503, Y=553 AND Y=580 WERE REPAIRED IAW SRM 53-05, 51-10-3 PAR 14 AND 21 AND 38.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,004 hrs · 46,886 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: STRUCTURE — CRACKED (LT WING) · airframe 63,004 hrs · 46,886 cycles

CRACKED PREVIOUS REPAIR ON LT WING L/E PRODUCTION DOUBLER STA XRS 164. DOUBLER WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (BS 1418) · airframe 63,004 hrs · 46,886 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, DOUBLER REPAIR ON FUSELAGE SKIN AT BS 1418 AND BETWEEN LONG 1-3L. DOUBLER REPAIR IS ATTENDED WITH ER/A 496150-14, REV ORIGINAL AND WILL BE INSPECTED PRIOR TO REACHING 56.250 TOTAL CYCLES.

Part: SEAT TRACK — CORRODED (BS 515-518) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK, X=54, STA Y=485 AND Y=515-518 AT PAX CABIN. DAMAGE WAS REMOVED, PLUGS AND AREAS WERE TREATED AND PAINTED AND PLUGS WERE INSTALLED IAW SRM 53-05, FIG 4A, SHEET 1, AND 51-10-3, PAR 14 AND 21.

Part: VANE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

RUSTED HARDWARE ON MID VANE OTBD FLAP AT LT WING. HARDWARE ON MID VANE OTBD FLAP AT LT WING WAS REMOVED AND INSTALLED NEW HARDWARE IAW AMM 20-30-01.

Part: INTERCOSTAL — CORRODED (BS 1200-1212) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

EXFOLIATIVE CORROSION ON INTERCOSTAL BTW LONGERON PROJECTION 19 RT STA Y1200 TO Y1212 AT UPPER DOOR JAMB C3. BEAM INTERCOSTAL WAS REMOVED NEW BEAM INTERCOSTAL WAS ADJUSTED, DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5, 51-10-3, 51-10-4.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,004 hrs · 46,886 cycles

WEAR ON DOUBLER FROM FWD LOWER CORNER AT FWD CARGO COMPARTMENT DOOR. DAMAGE DOUBLER WAS REMOVED IAW SRM 51-30-2. NEW REPAIR DOUBLER WAS FABRICATED IAW ERA. NR 486624-14MA, REV OG. REPAIR DOUBLER WAS TREAT AND PAINT IAW SRM 51-10-3, PAR 14/21. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,004 hrs · 46,886 cycles

WEAR ON REPAIR DOUBLER WEAR ON PRODUCTION DOUBLER FROM AFT LOWER CORNER AT FWD CARGO COMPARTMENT DOOR. DAMAGE DOUBLER WAS REMOVED IAW SRM 51-30-2. NEW REPAIR DOUBLER WAS FABRICATED IAW ERA NR 486624-14MA, REV ORIGINAL REPAIR DOUBLER WAS TREAT, PAINT IAW SRM 51-10-3, PAR 14/21. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: RIB — DAMAGED (RT WING) · airframe 63,004 hrs · 46,886 cycles

SCRATCH AFT BORE ON LT RIB STA XOS 580 AT SLAT PANEL NR 5 RT WING. DUE TO EXCEED ALLOWABLE LIMITS IAW SRM 57-02, PAR 9, TABLE 1 RIB XOS:580 N/P 9937564-2 THE SLAT PANEL NR 5 RT WITH N/P 5937563-502, N/S DL-64 WAS REPLACED.

Part: SEAT TRACK — CORRODED (BS 670-673) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK X 54 BETWEEN BS 670 - 673 AT PAX CABIN. SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: ANGLE — CRACKED (BS 120) · airframe 63,004 hrs · 46,886 cycles

TWO CRACKED ANGLES ON BS 120 BETWEEN X -54 TO -60 AND X 54 TO 60. ANGLES WERE REPLACED IAW SRM 51-30-2, SRM 51-30-5, DWG 9911559, REV A.

Part: SEAT TRACK — CORRODED (BS 638-643) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK X 54 BETWEEN BS 638 - 643. SEAT TRACK WAS REPAIRED IAW SRM-53-05, FIG 4A.

Part: RIB — SCRATCHED (RT WING) · airframe 63,004 hrs · 46,886 cycles

SCRATCH ON LEFT FWD BORE OF RIB XOS 198 AT SLAT PANEL NR 2 RT WING. DAMAGE WAS REWORKED AND MEASURED, WITH DIAMETER INBD 0.940, 1 HOLE, THEREFORE WITHIN LIMITS OF MAXIMUM REWORK HOLE DIAMETER IAW SRM 57-02, PAR 9 C, 1. BUSHING WAS FABRICATED IAW SRM 57-02, PAR 9C, 2.

Part: CUSP WEB — CRACKED (BS 241) · airframe 63,004 hrs · 46,886 cycles

CRACKED RT CUSP WEB AT BS 241 BETWEEN X -54 TO X -60 AT CABIN FLOOR STRUCTURE. DAMAGE WAS REMOVED. DOUBLER AND RING DOUBLER WERE FABRICATED. DOUBLER AND RING DOUBLER WAS TREATED AND PAINTED. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2, SRM 51-30-5, SRM 53-05, FIG 131A, SRM 51-10-3, PAR 14 AND 21.

Part: SUPPORT FITTING — CRACKED (BS 927) · airframe 63,004 hrs · 46,886 cycles

CRACKED FITTING SUPPORT BS 927, X 44 AND Z - 10. REMOVED FITTING AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, PAGE 1 AND 2 AND 51-10-3, PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 608-611) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK X 54, BS 608 - 611. SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A. NEW PLUG WAS ADJUSTED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-05 FIG 4A, APS 4.710-3 AND 51-10-3 PAR 14/21.

Part: IDLER LINK — CORRODED (SPOILERS) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BOLT AND BUSHINGS (2EA) TO REACTION LEVER AT RT INBD SPOILER ACTUATOR IDLER LINK. BOLT AND BUSHINGS TO REACTION LEVER AT RT INBD SPOILER ACTUATOR IDLER LINK WERE REPLACED.

Part: IDLER LINK — CORRODED (SPOILERS) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BOLT AND BUSHINGS (2EA) TO REACTION LEVER AT LT OUTBD SPOILER ACTUATOR IDLER LINK. BOLT AND BUSHINGS TO REACTION LEVER AT LT OUTBD SPOILER ACTUATOR IDLER LINK WERE REPLACED.

Part: RIB — CORRODED (RT WING SLAT) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION AFT BORE ON RT RIB STA XOS 83 AT SLAT PANEL NR 1 RT WING. DAMAGES WERE REWORKED AND FOUND WITHIN LIMITS IAW SRM 57-02 PAR 9. BUSHINGS WERE FABRICATED IAW SRM 57-02 PAR 9 C (2) AND INSTALLED IAW SRM 51-30-10 PAR 7.

Part: IDLER LINK — CORRODED (SPOILERS) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BOLT AND BUSHINGS (2EA) AT LT INBD SPOILER ACTUATOR IDLER LINK. BOLT AND BUSHINGS AT LT INBD SPOILER ACTUATOR IDLER LINK WERE REPLACED.

Part: RIB — CORRODED (NR 4 SLAT) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON BORE INNER AND OUTER SURFACE OF RIBS FROM STA XOS= 380 AND 429 AT LT SLAT PANEL NR 4. CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 26 WAS ACCOMPLISHED ORIGINAL THICKNESS ON RIB AT STA XOS=380 IS .270" AND MINIMUM REMAINING THICKNESS IS 0.259" WAS ACCOMPLISHED ORIGINAL THICKNESS ON RIB AT STA XOS= 429 IS 0.420" AND MINIMUM REMAINING THICKNESS IS 0.413" THEREFORE IT'S WITHIN OF LIMITS IAW SRM 57-01 FIG 1 REWORKED AREAS WRER TREATED AND PAINTED IAW SRM 51-10-3 PAR 14/21. DAMAGE ON STA XOS= 429 WAS REWORKED AND MEASURED, WITH I.D. HOLE 0.9365 (4 HOLES) THEREFORE WITH LIMITS OF MAXIMUM REWORK HOLE DIAMETER IAW SRM 57-02 PAR 9 C (1). BUSHINGS WERE FABRICATED (4 EAS) IAW SRM 57-02 PAR 9 C (2). DAMAGE ON RIB STA XOS= 380 WILL BE PERFORMED WITH CARD NO 16 A/C ZONE 11. AND BUSHINGS WERE INSTALLED IAW SRM 51-30-10 PAR 7.

Part: IDLER LINK — DAMAGED (SPOILERS) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON REACTION BOLT, BOLT, BUSHINGS AND CLEVIS TO REACTION LEVER AT RT OUTBD SPOILER ACTUATOR IDLER LINK. REACTION BOLT, BOLT, BUSHING AND CLEVIS TO REACTION LEVER AT RT OUTBD SPOILER ACTUATOR IDLER LINK WERE REPLACED .

Part: RIB — DAMAGED (RT WING SLAT) · airframe 63,004 hrs · 46,886 cycles

SCRATCH FWD BORE LT RIB STA XOS 186 AT SLAT PANEL NR 1 RT WING. DAMAGE REWORKED AND FOUND WITHIN LIMITS IAW SRM 57-02 PAR 9 C(1). BUSHINGS WERE FABRICATED IAW SRM 57-02 PAR 9 C(2) AND INSTALLED IAW SRM 51-30-10 PAR 7.

Part: SKIN — DAMAGED (BS 1418) · airframe 63,004 hrs · 46,886 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, DOUBLER REPAIR WITH ER/A 473483-14AD ON FUSELAGE SKIN AT BS 1418 BETWEEN LONGERONS 1-3R.

Part: ANGLE — CRACKED (BS 650) · airframe 63,004 hrs · 46,886 cycles

CRACK ON UPPER ANGLE FROM STA Y=650 AT MID CARGO COMPARTMENT DOOR. DAMAGED ANGLE WAS REMOVED IAW SRM 51-30-2. NEW ANGLE WAS DRILLED IAW SRM 51-10-4. PAR HOLES ON ANGLE WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21 PAR. ANGLE WAS INSTALLED IAW SRM 51-30-2.

Part: PAN — CRACKED (BS 598) · airframe 63,004 hrs · 46,886 cycles

CRACKED FWD UPPER ANGLE ON WINDOW RING PAN STA Y= 598 BELOW LONG 12 RT AT INTERNAL STRUCTURE. DAMAGE WAS REMOVED IAW SRM 53-05 FIG 122. REPAIR PARTS WERE FABRICATED IAW DC9/MD80 SRM 53-05 FIG 122. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 P21 AND 14. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: FORMER — CRACKED (VERTICAL STAB) · airframe 63,004 hrs · 46,886 cycles

CRACKED FORMER ON TIP FAIRING STA YV 172. REPAIR WERE FABRICATED IAW SRM 55-01 IG 4. DOUBLERS AND FILLERS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14-21. REPAIR INSTALLED IAW SRM 51-302.

Part: ANGLE — CRACKED (BS 185) · airframe 63,004 hrs · 46,886 cycles

CRACKED ANGLE OF INTERCOSTAL ON FWD MAIN ENTRANCE DOOR BETWEEN BEAM 4 AND 5 AND BS 185. ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE FABRICATED IAW DPS 4-710-3. TREATED AND PAINTED IAW SRM. 51-10-3 PAR. 14 AND 21. AND INSTALLED IAW SRM 51-30-2.

Part: PAN — CRACKED (BS 503-769) · airframe 63,004 hrs · 46,886 cycles

CRACK FOUND ON FWD UPPER LUG OF WINDOW RING PAN LH STA Y= 503, 927 AND 769. FWD UPPER LUG OF WINDOW RING PAN LH STA Y=503, 927 AND 769 WERE REPAIRED I.A.W. DC-9/MD80 SRM. 53-05 FIG. 122. AND ER/A 493648-14 MA, 487747-14 MA REV. ORIG. (LP1860721)

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,004 hrs · 46,886 cycles

DURING AN AD INSPECTION, A CRACK WAS FOUND ON FWD STOP FITTING NR 1 ON MID CARGO DOOR. STOP FITTING WAS REMOVED IAW SRM 51-30-5. NEW STOP FITTING WAS DRILLED, TREATED AND PAINTED, AND INSTALLED IAW SRM 51-10-4, SRM 51-10-3 PAR 21/14 AND SRM 51-30-5.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,004 hrs · 46,886 cycles

DURING AN AD INITIAL INSPECTION, A CRACK WAS FOUNDON AFT STOP FITTING NR 5 ON MID CARGO DOOR. STOP FITTING WAS REMOVED IAW SRM 51-30-05. NEW STOP FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-05, SRM 51-10-4 AND SRM 51-10-03 PAR 14/21.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,004 hrs · 46,886 cycles

CRACK FOUND ON AFT STOP FITTING NR 2 AT MID CARGO DOOR. STOP FITTING WAS REMOVED IAW SRM 51-30-05. A NEW STOP FITTING WAS DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-10-4, 51-10-3 PAR 21/14 AND SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 370-380) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB BTW X=-54 AND X=-60 FROM BS 370-380. DOUBLER AND FILLER WERE FABRICATED, TREATED, PAINTED, INSTALLED IAW SRM 51-10-3 PAR. 21, 14 51-70-4, 51-30-5.

Part: CUSP WEB — CRACKED (BS 731-750) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CRACK ON HOLE CUSP WEB BETWEEN STA Y=731 TO Y=750 AND BETWEEN X=55 TO X= 60 LT SIDE. CRACK WAS STOPPED IAW SRM 51-01, PAR 21 AREA WAS MEASURED IAW SRM 51-01, PAR 21, B. PARTS REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A-14 AND 51-30-2.

Part: PAN — CRACKED (BS 905) · airframe 63,004 hrs · 46,886 cycles

CRACK ON AFT LOWER LUG OF WINDOW RING PAN LT SIDE STA Y=905. REPAIRED IAW SRM 53-05 FIG 122 AND ER/A 493648-14 MA REV. ORIG. 487747-14 MA REV. ORIG.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,004 hrs · 46,886 cycles

CRACK ON AFT STOP FITTING NR 1 ON MID CARGO DOOR. STOP FITTING WAS REMOVED IAW SRM 51-30-05 NEW STOP FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-4, SRM 51-10-3 PAR 21/14 AND 51-30-05.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,004 hrs · 46,886 cycles

DURING AD INSPECTION, A CRACK WAS FOUND ON FWD STOP FITTING NR 5 ON MID CARGO DOOR. STOP FITTING WAS REMOVED IAW SRM 51-30-5. NEW STOP FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-4, SRM 51-10-3 PAR 21/14 AND 51-30-5.

Part: PAN — CRACKED (WINDOW) · airframe 63,004 hrs · 46,886 cycles

CRACK ON AFT UPPER LUG OF WINDOW RING PAN RT SIDE ON BS 946 - 1117. REPAIRED IAW SRM 53-05 FIG. 122, 51-10-3, 51-30-2, 51-30-5.

Part: BEAM — CRACKED (NR 1) · airframe 63,004 hrs · 46,886 cycles

CRACKED BEAM NR 1 FWD EDGE AT FWD MAIN ENTRANCE DOOR. REPAIRED IAW SRM 52-05 FIG 98.

Part: SEAT TRACK — CORRODED (BS 562-565) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON PLUG X=-22 BS 562-565, AT RT SEAT TRACK. PLUG WAS REPLACED IAW SRM 51-30-1, 53-05 FIG 4A, 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 454) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT CUSP WEB STA Y=454 BTW X=54 AND X=60. DOUBLER REPAR WAS FABRICATE, TREATED, PAINTED. INSTALLED IAW SRM 53-05 FIG 131A-14 51-10-3 PAR. 14, 21 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 335-357) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON RT CUSP WEB BETWEEN X=-54 AND X=-60 FROM STA Y=335-357 AT PAX CABIN. CUSP WEB BETWEEN Y 335-357, RT WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — DAMAGED (BS 636-712) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON CUSP WEB AND CLIPS BROKEN BETWEEN STA Y=636 TO Y=712 AND X=54 TO Y=60 LT SIDE. CUSP WEB ON Y=642-644 WAS ATTENDED WITH CARD 248, ZONE 201, NRC 20000048416. ON Y=698-706 WAS ATTENDED WITH CARD 250, ZONE 201, NRC 20000048417. CUSP WEB WITHIN LIMITS WAS REMOVED CORROSION AND TREATED AND PAINTED IAW SRM 51-10-3 PAR 26, 21, 14, 38. CLIPS WERE REPLACED IAW SRM 51-30-2,51-30-5 AND DWG 5913698, REV 1C. HFEC INSPECTION WAS PERFORMED ON REWORKED AREA. NO CRACK FOUND IAW ERA 511165-14MAR2015. MEASURE: ORIG 0.020" REMAINING ON STAY= 636 TO 643,Y= 645 TO 658, Y=660 TO 680, Y=682 TO 697, Y=702 TO 712 IS 0.018? WITHIN LIMITS.

Part: RETAINER — CORRODED (RUDDER) · airframe 63,004 hrs · 46,886 cycles

CORROSION ON SEAL RETAINER OF YOKE BEARING AT RUDDER MECHANISM. SEAL RETAINER WAS R & R AND WILL BE INSTALLED WITH CAR 2700-2126 AND JOB 001-0340, STEP NR 6. LP1856092.

Part: WASHER — CORRODED (TORQUE TUBE) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LOCK-WASHER OF RUDDER DRIVE TORQUE TUBE ASSY. LOCK-WASHER WAS R & R AND WILL BE INSTALLED WITH CARD 2700-2126 AND JOB 001-0340, STEP NR 7. LP1856088.

Part: YOKE — BROKEN (RUDDER) · airframe 63,004 hrs · 46,886 cycles

BROKEN YOKE BEARING OF RUDDER DRIVE TORQUE TUBE. BEARING WAS REMOVED AND WAS REPLACE AND WILL BE INSTALL WITH CARD 2700-2126 AND JOB 001-0340, STEP NR 8.

Part: CUSP WEB — CORRODED (BS 680-706) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT CUSP WEB BETWEEN X=54 TO X=60 FROM STA Y= 680-682 AND FROM STA Y= 698-706 AT PAX CABIN STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14, SRM 51-10-3 PAR 21 AND 14, SRM 51-10-5 AND 53-05, FIG 131A-14.

Part: CUSP WEB — CORRODED (BS 642-660) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON CUPS WEB BETWEEN STA X=54 AND X=60 FROM STA Y= 642-644 AND FROM STA Y=658-660 AT PAX CABIN STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 51-30-2, SRM 53-05, SRM 51-10-3 PAR 14 AND 21, SRM 51-30-5 AND 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (BS 569) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT CUSP WEB BETWEEN X=54 AND X=60 AND STA Y= 569 AT PAX CABIN STRUCTURE. CORROSION WAS REPAIRED IAW SRM 53-05, FIG 131A-13, SRM 51-10-3 PAR. 14, 21 & 38, SRM 51-30-2 AND SRM 51-30-5.

Part: ANGLE — CRACKED (WINDOW FRAME) · airframe 63,004 hrs · 46,886 cycles

CRACKED FWD UPPER ANGLE ON WINDOW RING PAN, STA Y=674 BELOW LONGERON 12RT AT INTERNAL STRUCTURE. WINDOW RING PAN, Y=674 WAS REPAIRED IAW SRM 53-05, FIG 122, SRM 51-30-2, AND 51-30-5. LP1856038.

Part: ATTACH FITTING — CRACKED (WINDOW FRAME) · airframe 63,004 hrs · 46,886 cycles

CRACK ON FWD LOWER LUG PF WINDOW RING PAN, RT SIDE ON STA Y=1041, 1060, 1136 AND 984. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE FABRICATED. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, P 21 AND 14, AND 53-05, FIG 122. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5. LP1856048.

Part: SEAT TRACK — CORRODED (BS 841-859) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK X=54, STA Y=841-843, Y= 857-859 AT CPAX CABIN. SEAT TRACK WAS REPAIRED WITH PLUGS IAW SRM 53-05, FIG 4A. LP1854712.

Part: SEAT TRACK — CORRODED (BS 841-859) · corrosion level 2 · airframe 63,004 hrs · 46,886 cycles

CORROSION ON LT SEAT TRACK, X=54 STA Y=841-843, Y= 857-859 AT CPAX CABIN. SEAT TRACK WAS REPAIRED WITH PLUGS IAW SRM 53-05, FIG 4A. LP1854467.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 63,004 hrs · 46,886 cycles

ON CUSP WEB BETWEEN STA Y=446 TO Y=465 AND BETWEEN X=54 TO X=60 LT SIDE. ALL CORROSION FOUND WAS REMOVED AND WAS IN LIMITS EXCEPT FOR CORRSION FOUND AT Y=454 WHICH WILL BE ATTENDED WITH CARD 256. LP1853423.

Part: CUSP WEB — CORRODED (BS 325-380) · airframe 63,004 hrs · 46,886 cycles

CORROSION RT CABIN FLOOR CUSP WEB FROM STA Y=325 TO Y=380 BETWEEN X=-54 TO X=-60. ALL CORROSION FOUND WAS REMOVED AND WAS IN LIMITS EXCEPT FOR CORRSION FOUND ON Y=335-357 WHICH WILL BE ATTENDED WITH CARD. LP1853430.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,943 hrs · 46,120 cycles

DURING CHECK, MAINTENANCE FOUND THAT SEAT 10D EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 61,812 hrs · 46,022 cycles

DURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE CABLE THAT RUNS BETWEEN THE LEFT UPPER AND LOWER SPADE LATCHES WAS FRAYED. MAINTENANCE REPLACED THE CABLE.

Part: FRAME — CRACKED (BS 1485) · airframe 61,799 hrs · 46,013 cycles

CANTED FRAME BS 1485 CRACKED AT INNER FLANGE AT AFT UPPER CORNER OF LT VENT BOX. WORKED ON NON ROUTINE 85. SUMMARY, CUTOUT DAMAGE. NEED HFEC CONTAINMENT. HFEC OF CUT OUT IAW NDT SPM 06-10-01.001, CONFIRM DAMAGE HAS BEEN CONTAINED. MADE DOUBLER AND TRIPLER IAW SRM 53-03D, FIG 48. OK TO INSTALL. REPAIR IS MOSTLY INSTALLED. W/W NR 128 COMPLETED INSTALLING FASTENERS IN REPAIR. VENT BOX FASTENERS WILL BE INSTALLED AT VENT BOX INSTALLATION. PAIRED IAW SRM 53-03D, FIG 48.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,407 hrs · 45,718 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE SEAT MOUNTED EMERGENCY LIGHT WAS INOPERATIVE AT SEAT 31D. MAINTENANCE REMOVED AND REPLACED THE WIRE HARNESS AND OPS CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 60,081 hrs · 44,814 cycles

DURING LINE CHECK, NOTED EMERGENCY PATH LIGHTS INOPERATIVE FROM ROW 31 AFT. REPLACED FUSE IN POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-53.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 59,689 hrs · 44,557 cycles

DURING LINE CHECK, SEAT 30D EMERGENCY LIGHT WIRE WAS NOTED TO BE FRAYED. WIRE HARNESS REPLACED IAW AMM 33-53 AND OPS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,677 hrs · 44,543 cycles

DURING LINE CHECK, EMERGENCY PATH LIGHTS IN AFT CABIN INOPERATIVE. FUSE IN THE AFT BATTERY PACK REPLACED AND OPS CHECKED NORMAL IAW AMM 33-53.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 58,048 hrs · 43,356 cycles

RIGHT WING FLAP T/E LOWER SURFACE DENTED. REPAIRED IAW SRM 57-01, FIG 1, SHT 2.

Part: BUSHING — WORN (TAILCONE) · airframe 58,048 hrs · 43,356 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE TEE PIN BUSHINGS WERE WORN BEYOND ALLOWABLE LIMITS. THE BUSHINGS WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: RELEASE MECH — DAMAGED (TAIL CONE) · airframe 58,048 hrs · 43,356 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CABLE, CABLE SLIDING BLOCKS, CAM RELEASE MECHANISM, TEE PIN BUSHINGS, LATCH HOUSING, AND LATCH SPRINGS WERE FRAYED, WORN, OR DAMAGED BEYOND ALLOWABLE LIMITS. THE ITEMS WERE ALL REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,869 hrs · 43,217 cycles

EMERGENCY LIGHTS INOP ROWS 31 TO 36 IN PASS SEATS. R & R BATTERY CHARGER OVER ROW 30 D/E, WORKED FOR 1 SEC THEN WENT INOP. SUSPECT BLOWN FUSE. SN ON 7239, SN ON 8481, MPN 11-0049. REPLACED AFT CABIN BATT CHARGER B5-212 AGAIN AND PERF OPS CK IAW AMM 33-53, OPS CK GOOD. OK FOR SVC.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,815 hrs · 43,173 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-36 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE ASSOCIATED FUSE AT THE POWER PACK CHARGER AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,738 hrs · 43,119 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-36 OF THE CABIN, THE EXIT IDENTIFIER AT THE AFT LT SERVICE DOOR, AND THE EEPL IN THE TAIL COMPARTMENT WERE ALL INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,569 hrs · 43,011 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,506 hrs · 42,980 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31 AND AFT IN THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 56,943 hrs · 42,559 cycles

THE PILOT REPORTS ONE COFFEE MAKER WAS EMITTING SPARKS AND CAUSED SMOKE IN THE GALLEY. THE COFFEEMAKER WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,277 hrs · 42,063 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE AFT EMERGENCY EXIT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: BUSHING — DAMAGED (TAIL CONE) · airframe 55,969 hrs · 41,829 cycles

DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, MAINTENANCE FOUND THE TEE PIN BUSHING, AS WELL AS THE LOWER CABLE CONDUIT DAMAGED, BEYOND ALLOWABLE LIMITS.

Part: SHUTOFF VALVE — INOPERATIVE (AC BAY) · airframe 54,699 hrs · 40,991 cycles

FLIGHT 1919 DIVERTED TO GRB FOR LOSS OF PRESSURIZATION. BOTH PACKS WERE INOPERATIVE. CREW BEGAN RAPID DESCENT AND ALL MASKS DEPLOYED. MAINTENANCE FOUND THE LEFT PACK INOPERATIVE. THE LEFT PRSOV WAS REPLACED PER THE AMM. LEFT AND RIGHT PACKS CHECKED OKAY.

Part: JACKSCREW — SHEARED (HORIZONTAL STAB) · airframe 54,457 hrs · 40,819 cycles

DURING PSV, PERFORMED FUNCTIONAL CHECKOUT OF HORIZONTAL STAB. ON POSTDOCK FOUND HORIZONTAL STAB NOT OPERATING AT FULL TRAVEL FOR NOSE UP. WHILE TROUBLESHOOTING AND OPERATING STABILIZER, THE FULL NOSE DOWN STOPS ON THE JACKSCREW CONTACTED AND SHEARED OFF. WORKED ON NRC 305 AND NRC 315. REPLACED JACKSCREW ASSY AND PERFORMED SYS RE-RIG.

Part: FRAME — CRACKED (BS 1485) · airframe 54,457 hrs · 40,819 cycles

BS 1485 FRAME CRACKED. REPAIRED IAW ERA 496701-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

DURING PSV, PAX MOD VISIT IN MSP FOUND AFT FUSELAGE TAIL CONE ATTACH FRAME STA 1510 CRACKED AT 2ND ALIGNMENT PIN BELOW UPPER RT LATCH ASSY. INSTALLED NEW FRAME SECTION PER MD88 SRM 53-03 FIG 802D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

DURING PSV, PAX MOD VISIT IN MSP FOUND AFT FUSELAGE TAIL CONE ATTACH FRAME STA 1510 CRACKED AT 1ST ALIGNMENT PIN ABOVE LOWER LEFT LATCH ASSY. INSTALLED DOUBLER REPAIR PER MD88 SRM53-03D FIG 802.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

AFT CARGO COMPARTMENT - CORROSION ON APB CHORD DOUBLER IN BILG AREA STA 1338 LBL 10-RBL 10. INSTALLED NEW DOUBLER PER MD88 SRM 53-05 FIG 115.

Part: FRAME — CORRODED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

WHILE IN MSP, MAINT NOTED CORROSION COMMON TO THE AFT PRESSURE BULKHEAD (APB) LOCATED AT APPROX S-27L TO S-27R. PERFORM FRAME ANGLE REPAIR PER MD88 SRM 53-05 FIG 93 PER ER/A 495945-14 REV ORIGINAL. REF A/C NR'S 218 AND 219.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

DURING PSV VISIT IN MSP FOUND FUSELAGE SKIN AROUND 2 RIVETS CRACKED AT STA 1437, 10 INCHES LEFT OF VERTICAL STABILIZER. REPAIRED PER ERA 496151-14. WORKED ON NRC 68.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

DURING PSV, PAX MOD VISIT IN MSP FOUND CRACK IN TAIL SECTION LONGERON 2L AT STA 1418. CUT OUT AND SPLICED IN NEW SECTION LONGERON PER MD88 SRM 53-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

DURING PSV VISIT IN MSP FOUND SKIN AROUND 3 RIVETS CRACKED AT STA 1418, 5 INCHES LEFT OF VERTICAL STABILIZER. REPAIRED PER ERA 496150-14. WORKED ON NRC 67.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,457 hrs · 40,819 cycles

DURING PSV, PAX MOD VISIT IN MSP FOUND AFT FUSELAGE TAIL CONE ATTACH FRAME STA 1510 CRACKED AT 3RD ALIGNMENT PIN BELOW LOWER RT LATCH ASSY. INSTALLED NEW FRAME SECTION PER MD88 SRM 53-03 FIG 802D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,381 hrs · 40,766 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 1CD INOPERATIVE. MAINTENANCE REPLACED PIG TAIL LIGHT ASSEMBLY AT 1CD. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,381 hrs · 40,766 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. MAINTENANCE REPLACED PIG TAIL LIGHT ASSEMBLY AT 19D. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 53,695 hrs · 40,257 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS WOULD NOT TEST FROM FORWARD F/A PANEL. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY PACK. OPERATION OF LIGHTS NOW CHECKS OK.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 53,583 hrs · 40,183 cycles

FUSELAGE PENETRATED IN UNPRESSURIZED SKIN ABOVE NR 2 PYLON DUE TO NR 2 ENGINE TURBINE FAILURE. REPAIRED PER DWG-SG09530001 REPAIR NOTE 3-ZONE 13. TEMP REPAIR, PERM REQUIRED WITHIN 8000 CYCLES FROM FLT 1976/09MAY2011. REP INSP REQD-DATA RETRIEVAL SENT.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 53,005 hrs · 39,827 cycles

MAINTENANCE FOUND EXTERIOR OVERWING EMERGENCY LIGHTS TURNED ON WHEN PERFORMING POWER TRANSFER. ALL EMERGENCY LIGHT SWITCHES WERE IN THE OFF POSITION. EXTERIOR LIGHTS TURN OFF AFTER CYCLING SWITCH BUT TURN BACK ON AT POWER TRANSFER. MAINTENANCE REPLACED BATTERY PACK AND RACK B5-49. LIGHTS OPERATE NORMAL. AIRCRAFT OKAY FOR SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 50,954 hrs · 38,457 cycles

EXFOLIATING CORROSION ON AFT CARGO COMPT LOWER DOOR JAMB BEAM FORM STA 1155 - 1212. REPAIRED IAW SRM 53-05.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,656 hrs · 38,256 cycles

SEAT ROW 2CD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CHECKS GOOD.

Part: DOOR — DAMAGED (MLG) · airframe 48,385 hrs · 36,746 cycles

DURING FCF RT MLG RED UNSAFE LIGHT ILLUMINATED AT 30,000 DURING CLIMB. PERFORMED QUICK REFERENCE HANDBOOK 14.8 PROCEDURE. AFTER THIS PROCEDURE THEN HAD A GEAR DOOR OPEN LIGHT ILLUMINATED. QUICK REFERENCE HANDBOOK 14.7. EMERGENCY LANDING WAS DECLARED AND A SAFE LANDING WAS ACCOMPLISHED. REMOVED AND REPLACED RT MLG DOOR AND PERFORMED ADJUSTMENTS AND OPS CHECKS PER DELTA OPN AND AMM.

Part: SKIN — DENTED (BS 200) · airframe 48,385 hrs · 36,746 cycles

SKIN DENT AT STATION 200 AT LONGERON 28R TO 29R. REPAIRED PER 53-04 FIG 12B SHEET 28 TO 30 PLATING REPAIR. REINSPECTION LIMITS 8000 LANDINGS ON AAR 202510.

Part: SKIN — DENTED (BS 237-256 L20L) · airframe 48,385 hrs · 36,746 cycles

DENT AT STATION 237 AND 256 LONGERON 20. REPLACED SKIN FROM STATION 229 TO 347.5 LONGERON 18L TO LONGERON 26L PER SRM 53-04 FIG 12C ON AAR 202106. REINSPECTION LIMITS 8000 LANDINGS CLASS 1 REPAIR.

Part: CUSP WEB — CORRODED (BS 1173) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB CORRODED AT STATION 1098 TO 1174 RBL 54. REPAIRED BY REPLACEMENT PER 51-30-05.

Part: CUSP WEB — CORRODED (BS 1155) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB CORRODED AT STATION 1155 RBL 54. REPAIRED BY REPLACEMENT PER 51-30-05 ON AAR 202871.

Part: CUSP WEB — CORRODED (BS 1137) · airframe 48,385 hrs · 36,746 cycles

RIGHT CUSP WEB CORRODED AT STATION 1137 RBL 54. REPAIRED BY REPLACEMENT PER 51-30-5.

Part: CUSP WEB — CORRODED (BS 1174) · airframe 48,385 hrs · 36,746 cycles

RIGHT CUSP WEB CORRODED OUT OF LIMITS AT 1174 AND RBL 54. REPAIRED BY REPLACEMENT PER 51-30-08.

Part: WEB — CORRODED (BS 1179) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB AT STATION 1079 CORRODED AT RBL 44. REPAIRED BY REPLACEMENT PER 51-30-05.

Part: SHEAR TIE — DAMAGED (BS 1437) · airframe 48,385 hrs · 36,746 cycles

FRAME SHEAR TIE AT STATION 1437 JUST OUTBOARD OF L2L AND L2R HAD MISSING FASTENERS. OPEN HOLES WERE INSPECTED, BACKDRILLED THROUGH THE DORSAL ATTACH ANGLE AND FASTENERS. INSTALLED PER ERA 473480-14 REV ORG. REPAIR IS TIME LIMITED AND TRACKED ON ACTL LINE NUMBER 2053.

Part: FRAME — CORRODED (BS 1060) · airframe 48,385 hrs · 36,746 cycles

LOWER HORIZONTAL FACING FLANGE OF FRAME AT STATION 1060 AND LONGERON 30R WAS FOUND CORRODED. TEMPORARY REPAIR INSTALLED PER ERA 473482-14 DUE TO NO AVAIL OF PART. PART WAS BLENDED AND HFEC INSPECTED, TREATED AND FRAME TO LONGERON FASTENERS REINSTALLED ON AAR NR 203014. TEMP REPAIR IS TRACKED ON ACT LINE NUMBER 2050.

Part: CUSP WEB — CRACKED (BS 243) · airframe 48,385 hrs · 36,746 cycles

RIGHT CUSP WEB AT STATION 243 RBL 44 CRACKED. REPAIRED PER ERA 470200-14 BY REPAIR PER DAC DRAWING SG09530003 REV B FIGURE 2, REPAIR IS TEMPORARY TO 12 MONTHS AND TRACKED ON ACTL LINE 2051. SAME REPAIR IS APPLIED BY THIS ERA TO STATION 1174 - 1250 LBL 54.

Part: MOUNT — CHAFED (NR 1 ENGINE) · airframe 48,385 hrs · 36,746 cycles

NUMBER ONE AFT LOWER MOUNT LUG CHAFING. REPAIRED PER ERA 46119-14 REV ORG BY BLENDING AND HFEC INSPECTION OF NACELLE REAR SPAR LOWER CAP AT STATION 1380. REMAINING MATERIAL .232 AND .231.

Part: DOOR FRAME — CORRODED (BS 1361) · airframe 48,385 hrs · 36,746 cycles

FLOOR SUPPORT FWD EDGE OF AFT ENTRY DOOR FRAME STA 1361 CORRODED UNDER SEALANT. REPAIRED VERTICAL DOOR JAMB ERA 457386-14 REV ORIG DATED 4/7/09.

Part: FRAME — CORRODED (BS 1098 S29-30L) · airframe 48,385 hrs · 36,746 cycles

FRAME CORRODED IN AFT PIT STA 1098 L29L-L30. REMOVED AND REPLACED FRAME IAW SRM 51-30-5.

Part: SHEAR TIE — CORRODED (BS 1271) · airframe 48,385 hrs · 36,746 cycles

SHEAR TIE ON FWD SIDE OF FRAME AT STA 1271 CORRODED BETWEEN LONG 18R AND 20R. REMOVED DAMAGE SHEAR TIE AND FABRICATED REPLACEMENT AND INSTALLED.

Part: FRAME — CORRODED (BS 1041) · airframe 48,385 hrs · 36,746 cycles

CORROSION ON FRAME AT FASTENER HOLES STA 1041 29L-30. REMOVED AND REPLACED FRAME STA 1041 L18L TO L18R IAW SRM 51-30-5 AND 51-30-2.

Part: MOUNT — WORN (NR 2 ENGINE) · airframe 48,385 hrs · 36,746 cycles

THE NACELLE REAR SPAR LOWER CAP AT FS 1380, NR 2 ENGINE AFT MOUNT LUG WAS FOUND WITH CHAFING ON THE FACES. THE WEAR WAS BLENDED AND FOUND ACCEPTABLE TO BOEING.

Part: MOUNT — WORN (NR 1 ENGINE) · airframe 48,385 hrs · 36,746 cycles

THE NACELLE REAR SPAR LOWER CAP NR 1 ENGINE AFT MOUNT LUG WAS FOUND WITH CHAFING. THE CHAFING WAS BLENDED AND FOUND TO BE ACCEPTABLE TO BOEING.

Part: SUPPORT FITTING — DAMAGED (MLG RETRACT ACT) · airframe 48,385 hrs · 36,746 cycles

RETRACT ACTUATOR SUPPORT FITTING AND BUSHINGS REPAIRED IAW 09-093855-03 C/W 09-093855-03 ME01 AND ME02

Part: ATTACH ANGLE — CRACKED (VERICAL STAB) · airframe 48,385 hrs · 36,746 cycles

VERTICAL STAB INTERNAL ATTACH ANGLE CRACKED AT FASTENER HOLE FWD END OF RAM AIR SCOOP. REPLACED INTERNAL ATTACH ANGLE PER 51-30-02.

Part: CUSP WEB — CORRODED (BS 598-712) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB CORRODED OUT OF LIMITS AT STATION 598 TO 712 LBL 54. REPAIRED BY REPLACEMENT PER 51-30-2.

Part: LONGERON — CORRODED (BS 294-313) · airframe 48,385 hrs · 36,746 cycles

STRINGER 28R CORRODED BETWEEN STATION 294 -313. REPAIRED PER SRM 53-02 FIRURE 19.

Part: FRAME — CRACKED (BS 1174) · airframe 48,385 hrs · 36,746 cycles

AFT CABIN FRAME 1174 CRACKED AT 5L AT GALLEY ATTACH FITTING. REPAIRED PER 51-70-05 FIG 1.

Part: SEAT TRACK — CORRODED (BS 593-690) · airframe 48,385 hrs · 36,746 cycles

SEAT TRACK CORRODED OUT OF LIMITS AT STATION 593 TO 690 AT LBL 22. REPAIRED BY SPLICE PER 53-05 FIGURE 4F SHEET 1 TO 11.

Part: SKIN — DENTED (BS 256 L19) · airframe 48,385 hrs · 36,746 cycles

DENT AT STATION 256 LONGERON 19 OUT OF LIMITS. REPAIRED PER 53-04D FIG 12B SHEETS 7 TO 9.

Part: CARGO TRACK — CORRODED (FWD CARGO BAY) · airframe 48,385 hrs · 36,746 cycles

FWD CARGO FLOOR TRACK CORRODED OUT OF LIMITS AT A STATION 785 TO 427 RBL17. REPAIRED BY REPLACEMENT PER 51-10-4.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 48,385 hrs · 36,746 cycles

THRESHOLD CORRODED AT MID CARGO DOOR ON PREVIOUSLY INSTALLED REPAIR. REMOVED DAMAGED REPAIR AND INSTALLED NEW THRESHOLD REPAIR PER 53-05 FIGURE 123 SHEET 1-12.

Part: CUSP WEB — CORRODED (BS 1109-1116) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB CORRODED AT STATION 1116 TO 1109 AT RBL 44. REPAIRED BY REPLACEMENT PER 51-30-05 ON AAR 203074.

Part: SKIN — DENTED (BS 229) · airframe 48,385 hrs · 36,746 cycles

SKIN DENT AT STATION 229 AT 27R. REPAIRED PER 53-04 FIG 12B SHEET 36.

Part: FRAME — CORRODED (BS 1098) · airframe 48,385 hrs · 36,746 cycles

FRAME CORRODED AT STATION 1098 AT 29L TO 30. REPAIRED BY REPLACEMENT PER 51-30-05 ON AAR 203042.

Part: ANGLE — CORRODED (BS 598-636) · airframe 48,385 hrs · 36,746 cycles

MID PIT RIGHT ZEE ANGLE CORRODED AT STATION 598 - 636. REPAIRED BY REPLACEMENT PER 51-30-0 ON AAR 202809.

Part: SKIN — GOUGED (BS 237) · airframe 48,385 hrs · 36,746 cycles

DENTS WITH GOUGES MEASURED OUT OF LIMITS PER 53-04 AT STATION 237 AND 256 JUST AFT OF L1 DOOR. INSTALLED REPAIR PER 53-14D FIG 12B SHEET 13-15 CLASS 1 REPAIR.

Part: LONGERON — CRACKED (BS 200) · airframe 48,385 hrs · 36,746 cycles

LONGERON 23L AT STATION 200 CRACKED. REPAIRED PER 53--2 FIGURE 18.

Part: SEAT TRACK — CORRODED (BS 231) · airframe 48,385 hrs · 36,746 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS AT STATION 321 RBL 22. REPAIRED BY REPLACEMENT PER 51-30-5 ON AAR 240659.

Part: ANGLE — CRACKED (BS 1350) · airframe 48,385 hrs · 36,746 cycles

AFT ENTRY DOOR WAY LOWER FRAME ANGLE CRACKED AT 1350 LBL8. REPAIRED PER 51-30-02.

Part: SUPPORT FITTING — CRACKED (BS 946) · airframe 48,385 hrs · 36,746 cycles

RT MLG DOOR ACTUATOR UPPER MOUNT TRAPEZOIDAL FITTING CRACKED AFT SIDE AT RADIUS. REPAIRED PER REPLACEMENT PER 51-30-05 ON NR 240818.

Part: SEAT TRACK — CORRODED (BS 1088-1309) · airframe 48,385 hrs · 36,746 cycles

SEAT TRACK AT STATION 1088 TO 1309 CORRODED OUT OF LIMITS. REPLACED TRACK PER 51-30-02 ON AAR 240654 AT LBL 44.

Part: CUSP WEB — CRACKED (BS 218) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB AT STATION 218 RBL 44 CRACKED. REPAIRED BY REPLACEMENT PER 51-30-01 ON AAR 241068.

Part: SEAT TRACK — CORRODED (BS 1114-1300) · airframe 48,385 hrs · 36,746 cycles

CABIN SEAT TRACK CORRODED OUT OF LIMITS. REPAIRED BY REPLACEMENT PER 53-05 FIG 4F AT STATION 1114 TO 1300 AT LBL 22.

Part: CUSP WEB — CORRODED (BS 807-905) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB AT STATION 807 TO 905 CORRODED. REPAIRED PER ERA 398191-14 MA REV A,ON AAR 240827.

Part: SHEAR TIE — CORRODED (BS 1287) · airframe 48,385 hrs · 36,746 cycles

SHEAR TIE AFT SIDE OF FRAME AT STATION 1287 CORRODED. REPAIRED BY REPLACEMENT PER 43-03D FIG 3 ON NR 202895.

Part: SEAT TRACK — CORRODED (BS 215) · airframe 48,385 hrs · 36,746 cycles

SEAT TRACK CORRODED OUT OF LIMITS AT STATION 215 RBL 54. REPAIRED BY REPLACEMENT PER 53-05 FIG 4F ON NR 240661.

Part: FRAME — CORRODED (BS 1309) · airframe 48,385 hrs · 36,746 cycles

FRAME AT STATION 1309 CORRRODED AT UPPER CORD. REPAIRED BY SPLICE PER 53-03D FIG 2A ON NR 202893.

Part: BEAM — CORRODED (CARGO DOOR WAY) · airframe 48,385 hrs · 36,746 cycles

AFT PIT CARGO DOOR CUT OUT LOWER BEAM CORRODED. REPLACED BEAM PER 53-05 FIG 123 ON NR 202911.

Part: RIB — CRACKED (LT WING) · airframe 48,385 hrs · 36,746 cycles

LEFT WIND LEADING EDGE RIB CRACKED AT XIS 136.421. REPAIRED PER DELTA ERA 464864-14 REV ORG DATED 3/17/09. FATIGUE CRACK WAS .5 INCHED AT THE LOWER FLANGE. REPAIR IS TEMPORARY WITH REQUIRED INSPECTIONS EVERY C CHECK.

Part: FLOOR SUPPORT — CORRODED (BS 424) · airframe 48,385 hrs · 36,746 cycles

FLOOR SUPPORT CORRODED AT STATION 424 IN FWD CARGO LBL 6. REPLACED SUPPORT PER 51-30-2 FIG 3 ON NR 240939.

Part: PANEL — CORRODED (LT WING) · airframe 48,385 hrs · 36,746 cycles

THE LT WING TDG OVERWING HEATER BLANKET NOFOD SYSTEM UPPER SKIN WAS FOUND WITH CORROSION REQUIRING BLENDOUT WITHIN A FEW INCHES OF THE PRIMARY BOOST PUMP ACCESS COVER. BLENDOUT RESULTED IN 3 SMALL HOLES THROUGH THE UPPER SKIN, EXPOSING THE PANEL CORE. THE DAMAGE WAS CLEANED UP, INSPECTED, AND REPAIRED PER THE APPLICABLE AMM 30-80-02-801 STEPS. THE PANEL IS THE SUBJECT OF AD 2002-21-06.

Part: SEAT TRACK — CORRODED (BS 512-785) · airframe 48,385 hrs · 36,746 cycles

MID CARGO FLOOR TRACK CORRODED AT STATION 512 TO 785. REPAIRED PER 51-30-01 BY REPLACEMENT ON NR 202672.

Part: SKIN — BULGED (FWD CARGO DOOR) · airframe 48,385 hrs · 36,746 cycles

FORWARD CARGO DOOR BULGED AFT CENTER. REPAIRED WITH DOUBLER PER 52-05D FIG 3 ON NR 203096.

Part: CUSP WEB — CORRODED (BS 588) · airframe 48,385 hrs · 36,746 cycles

STATION 588 CUSP WEB LBL 54 CORRODED OUT OF LIMITS. REPAIRED PER 53-05D FIG 827 ON AAR NR 242569.

Part: ATTACH BRACKET — CRACKED (KEEL BEAM) · airframe 48,385 hrs · 36,746 cycles

AFT END OF KEEL BEAM ATTACH BRACKET CRACKED. REPAIRED BY REPLACEMENT PER 51-30-05 ON NR 240590.

Part: CUSP WEB — CRACKED (BS 886) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB CRACKED AT STATION 886 LBL 54. REPAIRED PER ERA 398191MA REV A ON NR 241155.

Part: ATTACH BRACKET — CRACKED (KEEL BEAM) · airframe 48,385 hrs · 36,746 cycles

ATTACH BRACKET RIGHT AFT END CRACKED STATION 1003. REPAIRED BY REPLACEMENT PER 51-30-05 ON NR 240589.

Part: FLOOR SUPPORT — CORRODED (BS 165-200) · airframe 48,385 hrs · 36,746 cycles

FLOOR SUPPORT CORRODED AT STATION 165 TO 200 LBL 6. INSTALLED NEW FLOOR SUPPORT PER 51-30-05 ON NR 203512.

Part: SEAT TRACK — OUT OF LIMITS (STA 918) · airframe 48,385 hrs · 36,746 cycles

CABIN SEAT TRACK RBL 54 FS 918 FOUND TO BE OUT OF LIMITS. REPAIRED RBL 54 SEAT TRACK IAW SRM 53-05 FIG 4.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 48,385 hrs · 36,746 cycles

CABIN FLOOR SUPPORT CORRODED STA 200 LBL18 TO LBL38. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-2.

Part: BEAM — CORRODED (FS 1155-1212) · airframe 48,385 hrs · 36,746 cycles

AFT CARGO DOOR CUTOUT LOUVER BEAM CORRODED STA 1155-1212. REPAIRED BEAM IAW SRM 53-05 FIG 123.

Part: FLOOR SUPPORT — CORRODED (BS 162-195) · airframe 48,385 hrs · 36,746 cycles

CABIN FLOOR SUPPORT CORRODED AROUND NUTPLATES AT TOP AND BOTTOM SIDES STA 162-195 AT LBL 56. REMOVED AND REPLACED FLOOR SUPPORT.

Part: PULLEY BRACKET — CORRODED (LT ELEVATOR) · airframe 48,385 hrs · 36,746 cycles

LT ELEVATOR PULLEY SECTOR BRACKET CORRODED. REPLACED BRACKET.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,385 hrs · 36,746 cycles

CANTED FRAME 1485 RT SIDE FOUND TO BE CRACKED. REPAIRED PANEL AT CANTED FRAME 1485 IAW SRM 53-01 FIG 4.

Part: INTERCOSTAL — CORRODED (FS 784-788) · airframe 48,385 hrs · 36,746 cycles

MID PIT STA 784-788 BETWEEN L27L-28L I/B UPPER SIDE OF WEB CORRODED. REMOVED AND REPLACED INTERCOSTAL.

Part: SEAT TRACK — CORRODED (FS 915 - 1032) · airframe 48,385 hrs · 36,746 cycles

CABIN SEAT TRACK LBL22 FS915-1032 OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FIG 4F.

Part: FLOOR SUPPORT — CORRODED (FS 1220) · airframe 48,385 hrs · 36,746 cycles

AFT PIT LT FLOOR SUPPORT STA 1320-1220 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED FLOOR SUPPORT.

Part: SKIN — DAMAGED (STA 237 - 256) · airframe 48,385 hrs · 36,746 cycles

2 VERTICAL SCRATCHES IN DENTED AREA BETWEEN STA 237 AND 256 APPROX LONGERON 17L. INSTALLED REPAIR IAW SRM 53-04D.

Part: WEB — CRACKED (FS 218) · airframe 48,385 hrs · 36,746 cycles

SUB FLOOR MEMBRANE CRACKED AT FASTENER HOLE FS 218 RBL 44. REMOVED AND REPLACED FLOOR MEMBRANE SRM 51-30-2.

Part: SEAT TRACK — OUT OF LIMITS (FS 233-237) · airframe 48,385 hrs · 36,746 cycles

CABIN SEAT TRACK RBL 44 FS 233-237 FOUND TO BE OUT OF LIMIT. REMOVED AND REPLACED SEAT TRACK PER SRM.

Part: ANGLE — CRACKED (ACTUATOR MOUNT) · airframe 48,385 hrs · 36,746 cycles

CANT FRAME 1485 CRACKED RT SIDE UNDER RUDDER TRIM ACTUATOR MOUNT SECTOR. FABRICATED AND REPLACED ANGLE PER DWG 9911842.

Part: STRUCTURE — CORRODED (APU DOOR) · airframe 48,385 hrs · 36,746 cycles

RT APU ACCESS DOOR EDGE CORRODED. REPAIRED DOOR IAW SRM 52-05D FIG 10.

Part: CUSP WEB — CRACKED (STA 1090) · airframe 48,385 hrs · 36,746 cycles

CUSP WEB CRACKED FWD OF STA 1098 LBL 44. PERFORMED REPAIR PER ERA 398191-14MA.

Part: SKIN — DENTED (BS 200) · airframe 48,385 hrs · 36,746 cycles

DENT RT SIDE OF FUSELAGE BELOW R1 DOOR BETWEEN LONGERON 20 AND 21 STA 200. REPAIR INSTALLED DOCUMENTED ON AAR NR0014.

Part: FLOOR SUPPORT — CORRODED (STA 169-198) · airframe 48,385 hrs · 36,746 cycles

CABIN FLOOR SUPPORT CORRODED IN SEVERAL AREAS STA 169-198 RBL 54. REMOVED AND REPLACED CABIN FLOOR SUPPORT IAW SRM 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,385 hrs · 36,746 cycles

CABIN FLOOR SUPPORT CORRODED STA 192 LBL54. REPAIRED BY REPLACEMENT PER SRM 53-01 FIG 1.

Part: WEB — CORRODED (FUSELAGE) · airframe 48,385 hrs · 36,746 cycles

FWD CABIN FLOOR WEB CORRODED ON REPAIR DOUBLER STA 201 RBL 44. FABRICATED NEW WEB AND REINSTALLED. ACCOMPLISHED IAW SRM AND DWG 9936535.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,385 hrs · 36,746 cycles

FLOOR SUPPORT STA 427 STR 28L-28R GOUGED AND CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-2.

Part: ANGLE — CRACKED (APU BAY) · airframe 48,385 hrs · 36,746 cycles

APU SHROUD LEFT UPPER SURFACE FWD END CAP CRACKED. FABRICATED AND REPLACED END CAP IAW DWG 9915567.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 48,385 hrs · 36,746 cycles

AFT CARGO GUSSET CORRODED STA 1155 BETWEEN LONGERON 30 AND 29R. FABRICATED NEW GUSSET TO BE INSTALLED ON AAR NONROUTINE 1600-0587.

Part: SKIN — BENT (L1 DOOR) · airframe 48,385 hrs · 36,746 cycles

L1 DOOR LWR EDGE FLANGE BENT. FOUND TO BE LWR FWD EDGE APPROX 10 INCH LONG AND DOUBLER SEPARATED FROM SKIN. REPAIRED LWR DOOR SKIN IAW SRM 52-05D FIG 37.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 48,385 hrs · 36,746 cycles

FOUND SEAT TRACK LBL 44 FS 200 TO 246 WORN. INSTALLED NEW SEAT TRACK SECTION/SPLICE IAW SRM 53-05 FIG 4F.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,385 hrs · 36,746 cycles

FWD CARGO FLOOR SUPPORT STA 465 ABOVE LONGERON 29R CORRODED. REMOVED AND REPLACED CORRODED FLOOR SUPPORT IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (BS 724-727) · airframe 48,385 hrs · 36,746 cycles

CABIN RT CUSP WEB CORRODED AROUND OTBD LIGHTENING HOLE AT STATION 724 TO 727 AT RBL 54. REPAIRED POER 53-05D FIG 827D SHEET 1 ON AAR NR 0080.

Part: FLOORBEAM — CORRODED (BS 192) · airframe 48,385 hrs · 36,746 cycles

CABIN FLOOR SUPPORT CORRODED ON PSI WEB AT STATION 192 LBL 54. REPAIRED BY REPLACEMENT PER 53-10 FIGURE 1 SHEET 3 AND 51-30-2 ON AAR NR 0157.

Part: CUSP WEB — CORRODED (BS 511) · airframe 48,385 hrs · 36,746 cycles

LEFT CUSP WEB CORRODED SEVERAL AREAS BETWEEN STATION 511 TO 464 BOTH SIDES OF FLOOR TRACK AT LBL 54. REPAIRED PER 53005D FIGURE 827D SHEET 1 ON AAR NR 0092

Part: FLOORBEAM — CORRODED (BS 731) · airframe 48,385 hrs · 36,746 cycles

FLOOR SUPPORT CORRODED ACROSS FASTENER HOLES STATION 731 AT LONGERON 28L TO 28R. REPAIRD BY REPLACEMENT ON AAR 0148.

Part: STRAP — DAMAGED (BULKHEAD) · airframe 48,385 hrs · 36,746 cycles

P-DOME: EXTERNAL STRAP REPAIR IAW 09-086680-12. C/W 09-086680-12 ME13

Part: STRAP — DAMAGED (BULKHEAD) · airframe 48,385 hrs · 36,746 cycles

P-DOME: EXTERNAL STRAP & DRAIN HOLE BUSHING REPAIR IAW 09-093855-03. C/W 09-093855-03 ME01

Part: ENGINE — FAILED (NR 1) · airframe 45,513 hrs · 34,781 cycles

FLIGHTCREW REPORTED THAT EN ROUTE TO ATL LEFT ENGINE OIL FILTER CLOGGED MESSAGE ILLUMINATED ON OAP FOLLOWED BY THE LOSS OF OIL PRESSURE AND OIL QTY. FLIGHTCREW SHUT DOWN ENGINE AND DIVERTED TO STL. REPLACED NR 1 ENG PER TRANS 9T102.

Part: WIRE — BROKEN (NLG) · airframe 44,904 hrs · 34,382 cycles

ON DEPARTURE FROM MCO, RED NLG UNSAFE LIGHT REMAINED ILLUM WITH HANDLE UP NOSE GEAR IND PIN WAS FLUSH NO VIBES FELT PER CL LANDING HANDLE MOVED TO EXT POSITION NOSE GEAR REMAIN RED NLG IND PIN IND GEAR WAS DOWN AND LOCKED. BIT CHK OF PSEU IND FAULT CODE 457 NLG SENSOR DOWNLOCK WIRING FOUND AND REPAIR BROKEN SENSOR WIRE PSEU BITE CKS NML NLG SWUNG AND NOW CKS NORMAL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 43,711 hrs · 33,641 cycles

LEFT HYDRAULIC QTY DECREASED TO 3 QTS, PER PROCEDURE AFTER PUMP TURNED BACK ON LEFT PRESSURE REMAINED ZERO PUMP TURNED OFF. FOUND L1 LINE AT FILTER MODULE FWD FILTER WORN THROUGH BY A BOLT. REPLACED LINE PER AMM SPUN ENGINE LEAK CKS GOOD. SERVICED LEFT HYDRAULIC QTY TO FULL PER AMM OK FOR SERVICE.

Part: PROXIMITY SENSOR — WEAK (RT MLG) · airframe 42,274 hrs · 32,675 cycles

AFTER T/O RETRACTED GEAR RT LIGHT STAYED ON GEAR OPEN LIGHT WAS ILLUMINATED INTERMITTENTLY ALSO HAD AUTO SPOILER FAIL MSG GEAR EXT NORMAL ALL LIGHTS NORMAL EXCEPT STILL HAD SPOILER FAIL MSG. JACKED A/C, SWUNG GEAR. ALL INDICATIONS NORMAL. FOUND RT GEAR DOOR PROX SENSOR WEAK AND WORN BY USING ELDEC NO/GO GAUGES. REMOVED AND REPLACED RT GEAR DOOR PROX SENSOR PER M/M. RAN GEAR SEVERAL TIMES, ALL IND NORMAL CKS GOOD PER M/M 32-60-00.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 41,780 hrs · 32,332 cycles

EMERGENCY OVERWING EXTERNAL LIGHTS WILL NOT EXTINGUISH. REPLACED POWER SUPPLY.

Part: CHARGER — BURNED (MASTER BATTERY) · airframe 40,741 hrs · 31,601 cycles

AFTER T/O, SMELLED ODOR OF BURNT TOAST. ODOR DISSIPATED BY LEVEL OFF. FOUND BATTERY CHARGER WITH BURN SPOT ON IT. REPLACED BATTERY CHARGER BATTERYS AND BATTERY CHARGER C/B.

Part: SKIN — DAMAGED (BS 474) · airframe 37,959 hrs · 29,586 cycles

LIGHTNING STRIKE DAMAGE JUST FORWARD OF THE RIGHT ALTERNATE STATIC PORT. REPAIRED IAW ERA 093374-14, C/W ERA 093374-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,959 hrs · 29,586 cycles

LIGHTNING STRIKE DAMAGE FORWARD OF RIGHT ALTERNATE STATIC PORT .75 INCHES BY .25 INCHES.

Part: SHAFT — SHEARED (FUEL PUMP) · airframe 34,526 hrs · 27,197 cycles

RIGHT ENGINE FLAMED OUT AT APPROXIMATELY 60 KTS. MTC IN PROGRESS ON NR 2 ENGINE. FOUND FUEL PUMP SHAFT SHEARED. REPLACED PUMP AND CONTROL

Part: APU — LEAKING (APU BAY) · airframe 31,010 hrs · 24,652 cycles

STRONG BURNT ODOR FROM ROW 18 AFT. REPLACED APU FOR INTERNAL OIL LEAK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,822 hrs · 24,503 cycles

EMERGENCY TRACK LIGHTING FAILED TEST ROWS 1 THROUGH 12. REPLACED BATTERY PACK, OPS NORMAL.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 30,395 hrs · 24,191 cycles

AT 280FL NR 1 ENG HAD A COMPRESSOR STALL WITH VIBRATION. IT WAS FOLLOWED BY SMOKE IN THE CABIN. THE CREW KEPT THE ENG RUNNING UNTIL 3000 FT WHEN THE VIBRATION INCREASED. THE CREW THEN SHUT DOWN THE ENG REPLACED ENGINE.

Part: DUCT — RUPTURED (WATER SEPARATOR) · airframe 29,513 hrs · 23,520 cycles

FLOW LIGHT CAME ON DURING CLIMBOUT WHEN LEVEL AT 12000FT CABIN CONTINUED TO CLIMB THRU 8000 FT CABIN RATE UNCONTROLLABLE. FOUND RT WATER SEPERATOR AFT FLEX DUCT RUPTURED - REPLACED SAME

Part: DISPLAY — FAILED (COCKPIT) · airframe 29,459 hrs · 23,479 cycles

CREW REPORTS BURNED SMELL IN COCKPIT. FOUND RADAR DISPLAY BURNED, ALSO FOUND CAPTS MCDU OVERHEATED. REPLACED DISPLAY AND MCDU. CHECKS GOOD. ALSO REPLACED INST. COOLING FAN, ALL CHECK GOOD.

Part: STRUT — LEAKING (NLG) · airframe 28,490 hrs · 22,767 cycles

NOSE GEAR WOULD NOT RETRACT ON TAKEOFF. REPLACED STRUT PISTON. REPACKED AND SERVICED STRUT.

Part: ENGINE — FAILED (NR 1) · airframe 27,818 hrs · 22,254 cycles

ON T/O ROLL ADVANCED POWER ENGAGED AUTOTHROTTLES. LEFT ENGINE LOST POWER WITH ASSOCIATED BANG HEARD BY F/A. ABORTED TAKEOFF 50 KTS. LEFT ENGINE WOULD NOT ACCELERATE AFTER CLEARING RUNWAY. LOW OIL PRESURE LIGHT WAS ILLUMINATED AND EGT WAS 500C AT IDLE. FOUND DAMAGE TO FIRST STAGE FAN BLADES-COLDSTREAM FAIRINGS AT BLEED DUCT BETWEEN CORE AND OUTER CASE. REPLACED NR 1 ENGINE PER TRANS 9T102AD.

Part: SWITCH — STUCK (GEAR HANDLE) · airframe 26,916 hrs · 21,569 cycles

AFTER TAKEOFF GEAR HANDLE WOULD NOT RETRACT. FOUND SWITCH S1-89 STICKING. REPLACED SAME. LIGHTS CK OK WITH GEAR HANDLE. INSPECTED HANDLE AND GROUND SHIFT MECHANISM, NOSE GEAR AND STRUT. CHECKS GOOD. SERVICED NOSE STRUT PER M/M, JACKED AIRCRAFT AND RAN GEAR SEVERAL TIMES. ALL GEARS OPERATE NORMALLY. ALL GEAR INDICATIONS CHECK NORMAL.

Part: COALESCER — CONTAMINATED (CABIN)

ON TAXI OUT IN CVG, FWD LAV SMOKE DETECTOR CAME ON AND AN ODOR WAS DETECTED IN THE FORWARD PORTION OF THE CABIN. ALSO, PASSENGERS REPORTED SMELLING SMOKE. PERFORMED DUCT BURNOUT, REPLACED COALESCERS.

Part: INLET — DIRTY (APU)

RETURNED TO GATE AFTER SMOKE DETECTORS (BOTH AFT LAVS) WENT OFF. LEFT ENG RUNNING, LEFT PACK RUNNING FOR 5 MIN. APU AIR RUNNING, RIGHT PACK RUNNING SINCE PUSHBACK (20 MIN). LIGHT SMOKE (HAZE VISABLE IN REAR OF CABIN). CLEANED APU INLET BOX, PERFORMED DUCT BURNOUT.

Part: INLET — CONTAMINATED (APU)

AFTER TAKEOFF AT ABOUT 4,000 FEET, EXPERIENCED SMOKE IN THE CABIN. ALL 3 LAV SMOKE DETECTORS WENT OFF, RETURNED TO ATL. CLEANED APU INLET, PERFORMED DUCT BURNOUT.

Part: DFGC — FAILED (E/E COMPT)

SHORTLY AFTER TAKEOF, LOST BOTH FLT DIRS, SEVERAL AMBER LIGHTS ON COMPARATOR CAME ON AND A/P WOULD NOT ENGAGE. SHORTLY AFTER, SMELLED A STRONG ACRID ODOR. CKD COCKPIT AND ELECTRONIC BAYS FOR EVIDENCE OF ELECTRICAL PROBLEMS, NONE FOUND. PERFORMED RTS ON NR 1 DFGC CKD GOOD. PERFORMED RTS ON NR 2 DFGC, FAILED NR 2 DFGC AIL MECH TORQUE SW. REPLACED NR 2 DFGC RTS GO. RAN ENGS TO T/O. POWER, NO PROBLEMS NOTED.

Part: FUSE HOLDER — LOOSE (NR 2)

ON TOUCHDOWN, C/B POPPED ELECTRICAL FUMES IN COCKPIT AT GATE FOUND DFGC-1 POPPED, RESET IT POPPED W/FUMES. FOUND F/O FMA F2 FUSEHOLDER LOOSE SHORTING TO GROUND.

Part: FLT MGT COMPUTER — FAILED (E/E COMP)

AFTER T/O, NR 1 DFGCS CB POPPED AND FAILED, SMOKE AND ELEC SMELL WAS NOTICEABLE. SMOKE WAS VISABLE NEAR GEAR HNDL AND MODE ANNUN PNL.

Part: SKIN — CRACKED (E/E DOORWAY)

THE FUSELAGE SKIN AND UNDERLYING INTERNAL DOUBLER WERE FOUND CRACKED AT STR 29R, APPROXIMATELY 10 AFT OF THE E/E DOOR. A 2 INCH BY 1 INCH CUTOUT IN THE SKIN AND DOUBLER WAS REQUIRED TO REMOVE THE DAMAGE. THE ORIGINAL SKIN IS MANUFACTURED FORM 0.050 2024-T3 AND THE INTERNAL DOUBLER IS MANUFACTURED FORM 0.063 2024-T42.

Part: FLOOR MEMBRANE — CRACKED (BS 1290)

SUB-FLOOR MEMBRANE CRACKED LT AND RT SIDE AT STA 1290. REPLACED LT AND RT MEMBRANE PER SRM 53-05 FIG 100.

Part: BUSS PROTECT PNL — MALFUNCTIONED (E/E COMPT)

AFTER TAKEOFF, CROSS TIE LOCKOUT, GEN AND OR CROSSTIE RELAY CHATTER. TURNED OFF LEFT GEN, RETURNED DFW. REPLACED BUS PROTECTION PANEL, OPERATION NORMAL.

Part: SKIN — CRACKED (FWD FUSELAGE)

DURING E-2 LETTER CHECK, FOUND SKIN CRACKED AT LT NLG STRUT DOOR AFT HINGE CUTOUT. REPAIRED PER SRM 53-05 FIG 62A.

Part: SKIN — CRACKED (FWD FUSELAGE)

DURING E-2 LETTER CHECK, FOUND SKIN CRACKED AT RT NLG STRUT DOOR AFT HINGE CUTOUT. REPAIRED PER SRM 53-05 FIG 62A.