N916DL

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 82,697 hrs · 63,504 cycles

EMERGENCY LIGHTS OUT AT L1 AND R1 DOORS AND SEATS 1C TO 12D. FOUND FUSE BLOWN ON POWER SUPPLY AT SEAT 3D. REPLACED FUSE. OPS CHECK OK. REFERENCE MD-88 CMM 33-21-70. PN ON B215-06. (LP6030176)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 82,683 hrs · 63,490 cycles

ON SHORT FINAL WE HEARD A BEEPING NOISE IN BACK IT APPEARS THE LAV SMOKE DETECTOR DISCHARGED NO EVIDENCE OF FIRE. INSP BOTH REAR & FWD LAV SMOKE DETECTORS, FIRE BOTTLES & TEMP PLACARDS. NTF. DUE TO PILOT REPORT TO MCC OF A TYPE SMELL AT FWD LAV, PLACED ON MCO IAW MEL 26-00-06B, M PROCEDURE C/W. PLACARD INSTALLED. MCC (TOM) NOTIFIED < FIRE EXTINGUISHER. (LP6030154)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,667 hrs · 63,481 cycles

WORKING SERVICE CHECK FOUND EMERGENCY LIGHT (L1 EXIT, R1 EXIT AND FIRST CLASS LIGHT) INOP. REMOVED AND REPLACED EMERGENCY POWER SUPPLY B5 -211 AND BATTERY ASSY PER MD88 AMM 33-53 OPS TEST GOOD. (LP6030148)

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 82,630 hrs · 63,446 cycles

DURING SVC FOUND SEAT 35ED EMERGENCY LIGHT INOP. FOUND WIRE PULLED FROM PIN REMOVED AND REPLACED EMERGENCY LIGHT PIN PER MD88 SWPM 20-90-03 AT SEAT 35ED OPS CHECK GOOD. (LP6030101)

Part: SUPPORT — CRACKED (NR 1 NACELLE) · airframe 82,079 hrs · 62,914 cycles

NR 1 ENG PYLON INTERNAL SUPPORT INTERCOSTAL CRACKED @ UPPER & LOWER FASTENERS (JUST AFT OF 13TH STAGE DUCT CONN.). REMOVED INTERNAL SUPORT. INSTALLED NEW INTERNAL SUPPORT (SHIELD) P/N 9935719-5 REF DWG 5935702. (LP1233384)

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 81,762 hrs · 62,626 cycles

L/R THRUST REV SCRAPED ON LANDING. REMOVED T REPLACED #1 ENG THRUST REVERSER ASSY PER MD88 AMM 78-30. REVERSER, THRUS OFF 03-7831-9-0081 00171 ON 03-7831-9-0081 10110. (LP5772838)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,667 hrs · 62,545 cycles

FOUND EMERGENCY LIGHTS IN FIRST CLASS CABIN SECTION INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK PER MD88 AMM 33-53. (LP #4694868)

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 81,395 hrs · 62,304 cycles

CLB PWR @ APPROX 6500 CLIMBING RT OIL QUANTITY WENT TO ZERO FOLLOWED BY RT OIL LOW MESSAGE. FOLLOWED QRH AND SHUT DOWN PER CHECKLIST. NO ABNORMAL APPROCH AND LANDING INTO MCO. OIL PX WENT TO ZERO FOR APPROX 2 MIN. REMOVED AND REPLACED NR 2 ENGINE PER WC 7100-4682-RH ACFT OK FOR SVC. ALL RII COMPLIED WITH. POWER PLANT, JT OFF 88-7110-9-0010 18124 ON 88-7110-9-0010 18128. (LP5474516)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,204 hrs · 62,132 cycles

EMERGENCY LIGHTS INOP ROWS 1-12. REMOVED AND REPLACED BATTERY PACK AT LOCATION B5-211 AND PERFORMED OPS CHK OF EMERGENCY ESCAPE PATH LIGHTING AS PER AMM 33-53. CHECKS OK. (LP5759083)

Part: SKIN — DELAMINATED (TE FLAP VANE) · airframe 81,139 hrs · 62,073 cycles

AWR IN REF, MON/916/012-MON, 88 REP, 2855432. DELAMINATED WAS FOUND ON RT OUTBOARD FLAP, MID FLAP VANE UPPER SKIN (AD). RT OUTBOARD FLAP, MID FLAP VANE UPPER SKIN WAS REPAIRED PER SRM 57-03D PAR.11 B (2) AND (UT) TAP-TEST INSPECTION WAS ACCOMPLISHED ON RT OUTBOARD FLAP, MID FLAP VANE UPPER SKIN AND NO DISBONDED WERE FOUND AFTER REPAIR PER, SRM 51-70-2 PAR. 14. A. (LP0988523)

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,135 hrs · 62,071 cycles

INITIAL INSPECTION: CRACK AND GOUGE ON FUSELAGE SKIN ON JACK POINT HOLE BETWEEN LONGERONS 30 AND 29R STA. 218. PERMANENT REPAIR SECTION I WAS PERFORMED ON FUSELAGE SKIN AT JACK POINT HOLE BETWEEN LONGERONS 30 AND 29R STA. 218. PER ER/A 576284-14 REV.ORIGINAL AND ETI -88-19-023 REV.1. PERFORM INSPECTION CHECK WITHIN EVERY 8,000 CYCLES AFTER INSTALLATION OF SECTION I: PERMANENT REPAIR, FOLLOWED WILL BE PERFORMED UNDER LOG PAGE # 0981536. (LP0986355)

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,135 hrs · 62,071 cycles

AWR IN REF MON/916/096-MON, 88 L.P. 0582257: DURING INSPECTION WAS FOUND CRACK ON FUSELAGE SKIN STA Y=1437 BTW LONG 3R TO 4R NEAR TO PREVIOUS REPAIR. FUSELAGE SKIN WAS REPAIRED (PERMANET REPAIR) PER ER/A 576322-14 REV ORIGINAL AND ETI-88-19-024 REV 2. GENERAL VISUAL INSPECTION WILL BE MONITORING EVERY 3000 CYCLES UNDER L.P. 0981693. PER ERA 576322-14 REV. . ORIGINAL. SECTION II. (LP0983643)

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,135 hrs · 62,071 cycles

CRACK ON FUSELAGE SKIN LONGERON 10 RH BETWEEN STA.207 AND 218. FUSELAGE SKIN WAS REPAIRED (PERMANET REPAIR) PER ER/A 576287-14 REV ORIGINAL AND ETI-88-19-022 REV. 2 GENERAL VISUAL INSPECTION ON REPAIR WILL BE MONITORING EVERY 8000 CYCLES UNDER L.P. 0981635 PER ERA 576287-14 REV ORIGINAL SECTION II. (LP0983470)

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 81,135 hrs · 62,071 cycles

INITIAL INSPECTION: CRACK ON SKIN APROX STA 916 BELOW CUT OUT THROUGH ACCESS PANEL 630 1 A AT VERT. EST. SKIN APROX STA 916 BELOW CUT OUT THROUGH ACCESS PANEL 6301 A AT VERT. EST. WAS REPAIRED PER SRM 55-05 FIG.3. (LP0977861)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,969 hrs · 61,933 cycles

GALLEY AND FIRST CLASS EMERGENCY LIGHTS INOP. R/R POWER SUPPLY/ BATT CHARGER FUSES PER MD 88 AMM 23-51. OPS GOOD. (LP5571308)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 80,939 hrs · 61,905 cycles

EMERGENCY EXIT AND PATH LIGHTS ROW 1-12 IN OP. T/S EMERGENCY LIGHTS IAW AMM 33-53, R/R BATTERY POWER SUPPLY, P/N RPS1B, S/N OFF 032, S/N ON 6830, OP CKS GOOD IAW AMM 33-53. (LP5242190)

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 80,776 hrs · 61,767 cycles

L ENG FAIL AT 35K CRUISE ALT NO WARNING PRIOR N2 READ 0 TEMP NORMAL NO FIRE NO RESTART ATTEMPTED DUE TO N2 READING ZERO. REMOVED & REPLACED NR 1 ENG IN REF. TO W/C 7100-4682-LH REF. LOG 891850. (LP4578987)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,545 hrs · 61,584 cycles

L1 & R1 DOOR EMERGENCY LIGHTS INOP. RELAMPED EMERGENCY LIGHTS AT L1 & R1 DOOR PER MD88 33-51 OPS CK NML. (LP5037658)

Part: BEARING — FAILED (NLG WHEEL) · airframe 80,536 hrs · 61,574 cycles

LT NOSE WHEEL BEARING FAILURE. REMOVED BOTH NLG TIRES AND SPRAY DEFLECTORS PER MD88 AMM 32-40. REMOVED & REPLACED NLG PISTON PER MD88 CMM 32-21-1 DAL REV #62. INSTALLED BOTH NLG TIRE ASSY'S AND SPRAY DEFLECTORS PER MD88 AMM 32-40. C/W NLG STRUT SERVICING AMDS W/C 3221-6444. SDR REPORTED DUE TO FACT THAT NUMBER ONE ENGINE SUFFERED DAMAGE FROM THE BEARING FAILURE ON LOGSHEET 5037654. (LP5037653)

Part: BEARING — FAILED (NLG WHEEL) · airframe 80,536 hrs · 61,574 cycles

LT ENGINE FOD MULTIPLE BLADES AND LINER. NBR 001 ESN 718214 REPLACED IAW AMDS W/C 7100-4682-LH. REF LOG 0843278. SDR REPORTED DUE TO LEFT NOSE TIRE BEARING FAILURE ON LOGSHEET 5037653 CAUSEING THE DAMAGE TO THIS ENGINE. (LP5037654)

Part: HOLDER — FAILED (EMERGENCY LIGHTS) · airframe 80,380 hrs · 61,436 cycles

FOUND ROW 1C TO 12C EMERGENCY LIGHTS INOP DURING SERVICE CHECK. TROUBLESHOT PER MD-88 AMM 33-53. FOUND BATTERY HOLDER AT 3D BAD. REMOVED AND REPLACED BATTERY HOLDER PER MD-88 AMM 33-53. ALL CHK GOOD. OK FOR SERVICE. (LP4665963)

Part: FUSE — BLOWN (CABIN) · airframe 80,312 hrs · 61,365 cycles

ALL EMERGENCY EXIT LIGHT IN F/C AND FWD ENTRY INOP. TROUBLESHOT FWD SECTION EMERGENCY LIGHTS FOUND B5-211 BATTERY PACK OVER ROW 3 CD FUSE BAD REPLACED PER WIRING DIAGRAM MAN 33-51-14. CKS GOOD PER AMM 33-53-01.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 80,290 hrs · 61,347 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT PATHING IN THE BUSINESS CLASS AND ROWS 10-13 WERE INOPERATIVE. TROUBLE SHOOTING PER WDM 33-51-14 LEAD TO AN INOPERATIVE POWER SUPPLY CIN B5-211. THE POWER SUPPLY WAS REPALCED PER WDM 33-51-14. OPERATIONAL CHECK WAS GOOD. (LP 4665909)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 80,101 hrs · 61,191 cycles

THE FORWARD EMERGENCY PATH LIGHTS WERE FOUND TO BE INOPERATIVE DURING A SERVICE CHECK. MAINTENANCE FOUND THE POWER SUPPLY AND BATTERY TO BE BAD. THE POWER SUPPLY AND BATTERY WERE REPLACED PER AMM 33-53. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 79,991 hrs · 61,091 cycles

FWD CABIN EMERGENCY LIGHT BATTERY PWR SUPPLY INOP. REPLACED BATTERY PWR SUPPLY REF AMM 33-53. OP CK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,886 hrs · 60,993 cycles

ROWS 1 - 12 AND FWD ENTRANCE DOORS EMERGENCY LIGHTS WERE INOPERATIVE. TROUBLESHOT IAW SRM 33-51. REPLACED THE BATTERY PACK B5-211 IAW AMM 33-53. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 79,788 hrs · 60,913 cycles

SEVERAL EMERGENCY CABIN LIGHTS WERE INOPERATIVE. SEAT ROWS 1 - 12 AND 24 - 30 SEAT LIGHTS INOPERATIVE AND MULTIPLE CEILING LIGHTS THRU CABIN AND 1/2 EMERGENCY EXIT SIGNS AT OVER WING DOOR INOPERATIVE. TROUBLESHOT IAW WDM 33-51, FOUND EMERGENCY LIGHT WIRE BROKEN AND SHORTED AT SEAT ROW 29. REPAIRED THE WIRE IAW WSPM 20, ALSO REPLACED SEVERAL BULBS THROUGHOUT THE CABIN SYSTEM CHECKED GOOD.

Part: CRADLE — DEFECTIVE (CABIN) · airframe 79,742 hrs · 60,875 cycles

DURING SERVICE FOUND ROWS 1-4 AND 10-13 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY POWER SUPPLY CRADLE PER AMM 33-50 OPS CHECK GOOD ACFT IS OKAY FOR SERVICE.

Part: PIN — BROKEN (EVAC SLIDE) · airframe 79,727 hrs · 60,863 cycles

PIN BROKEN ON SLIDE BUSTLE GALLEY DOOR. INSTALLED NEW SLIDE PER CARD 2561-49647.

Part: TURBINE — DAMAGED (LT ENGINE) · airframe 79,487 hrs · 60,671 cycles

DIVERTED TO TLH DUE TO LEFT ENGINE COMPRESSOR STALL. THE ENGINE WAS SHUTDOWN. MAINTENANCE FOUND TURBINE DAMAGE AND THE LEFT ENGINE WAS REPLACED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 79,429 hrs · 60,621 cycles

FIRST CLASS AND FWD GALLEY EMERGENCY LIGHTS INOP. R&R FWD BATTERY CHARGER PER AMM 33-50. OPS CHK GOOD.

Part: CABLE — FRAYED (TAILCONE) · airframe 79,411 hrs · 60,607 cycles

TAILCONE KEVLAR CABLE FRAYED. REPLACED TAILCONE KEVLAR CABLE REF ROUTINE CARD 5350-01077-0101.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,411 hrs · 60,607 cycles

FIRST CLASS UPPER EMERGENCY LIGHT INOP. REMOVED AND INSTALLED NEW EMERGENCY BATTERY PACK IAW AMM 33-53-00, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 79,402 hrs · 60,599 cycles

UPON SVC CK FOUND ROWS 1 CD THRU 12 ED EMERGENCY PATH LIGHTING INOP. R&R BATTERY POWER SUPPLY FWD CABIN PER WDM 33-51-12. ALSO R&R BATTERY ASSY (FWD CABIN) PER 33-53 OPS CKS NML A/C OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 79,288 hrs · 60,511 cycles

ON SVC CK FOUND FIST CLASS EMERGENCY LIGHTS INOP. R&R FUSE AT BATTERY CHARGER IN O/H COMP ABOVE 2 CD PER WDM 33-51 AND OPS CK PER AMM 33-53 OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,214 hrs · 60,453 cycles

FWD EMERGENCY LIGHTS ON FIRST CLASS OVERHEAD NOT TURNING ON. REPLACED BATTERIES PER 33-53, NO HELP. RELAMPED ALL OVERHEAD EMERGENCY LIGHTS REF AMM 33-53. OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,410 hrs · 60,606 cycles

FIRST CLASS UPPER EMERGENCY LIGHTS INOPERATIVE. INSTALLED A REPLACEMENT BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.

Part: DIODE — FAILED (EMERGENCY LIGHTS) · airframe 79,050 hrs · 60,321 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED A BAD DIODE ON THE BATTERY CARTRIDGE RECEPTACLE IAW AMM 33-50. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,983 hrs · 60,270 cycles

FIRST CLASS EMERGENCY CEILING LIGHTS NOT WORKING. RESET EMERGENCY LIGHTING SYSTEM IAW AMM 33-53. LIGHTS WORK OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,706 hrs · 60,046 cycles

ON PDC FORUM ROW 1-12 EMERGENCY PATH LIGHTS INOP. R&R BATTERY AND BATTERY CHARGER PER AMM 33-53. OPS NML. OK FOR SVC.

Part: APU — ODOR (APU BAY) · airframe 78,618 hrs · 59,976 cycles

UPON ARRIVAL IN YYZ AFTER STARTING APU DURING TAXI TO GATE GOT A STRONG RAW FUEL ODOR THROUGHOUT CABIN. CREW ALSO SMELLED IN COCKPIT. PASSENGERS COMPLAINED OF FUMES. THE APU WAS REPLACED AND DOCUMENTED ON LP 9983360.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,612 hrs · 59,972 cycles

COCKPIT OVERHEAD AND FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOP. RE LAMPED IAW MM 33-50 AND ALL LIGHTS OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,332 hrs · 59,748 cycles

ON S/C FOUND FC EMERGENCY LIGHTS INOP. T/S R&R F/C BATTERY ASSY. OPS CHECKS GOOD AS PER AMM 33-53.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 78,240 hrs · 59,689 cycles

AFT STAIR OVERHEAD EMERGENCY LIGHT INOPERATIVE. TERMINATED A LOOSE WIRE. CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,087 hrs · 59,564 cycles

SEATS 1 - 11 EMERGENCY LIGHTS INOPERATIVE. R & R THE POWER SUPPLY AND BATTERY IAW AMM 33-20, CHECKED GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,041 hrs · 59,530 cycles

CABIN EMERGENCY LIGHTS AT CEILING BETWEEN SEATS 22 THROUGH 25 INOPERATIVE. REPLACED THE BATTERY PACK BP5104, CHECKED GOOD IAW AMM 33-53.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,827 hrs · 59,330 cycles

MAIN ENTRANCE AND FWD SERVICE DOOR EXIT IDENTIFIER LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-53, OPS CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 77,821 hrs · 59,324 cycles

FOUND SEATS 1-12 EMERGENCY LIGHTS INOPERATIVE. REPLACED THE FUSE IN THE BATTERY PACK IAW WIRING DIAGRAM MANUAL 33-51-14 PG. 506. OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,539 hrs · 59,080 cycles

EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT THE FIRST CLASS EMERGENCY LIGHTS IAW AMM 33-53. REPLACED THE BATTERY AND CHARGER IAW AMM 33-53. OPS CHECKED GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 77,492 hrs · 59,040 cycles

F/C EMER LIGHTS INOP ON TEST. REPLACED FUSE AT BATTERY PACK B5-211. OPS CHECK GOOD REF WDM 33-51-14.

Part: HOUSING — CRACKED · airframe 76,222 hrs · 58,049 cycles

CRACKED SPRING HOUSING AT VENTRAL MOVABLE CEILING. THE SPRING HOUSING WAS REPAIRED IAW ER/A 554171-14, REV. ORG. AND ETI-88-17-074, REV. 1.

Part: STRINGER — CRACKED (RT WING) · airframe 76,222 hrs · 58,049 cycles

RIGHT WING CRACKED STRINGER 17R, XWC=15. THE STRINGER AND FWD SKIN WERE REPAIRED IAW ER/A 554113-14MA REV. ORIG. AND ETI-88-17-027 REV. 3.

Part: PAN — CRACKED (CARGO DOOR) · airframe 76,222 hrs · 58,049 cycles

CARGO DOOR CRACKED ON OUTER PAN LOWER EDGE BETWEEN BS 654 - 658 AND BS 670 - 677. THE PAN WAS REPAIRED IAW ETI-88-17-061 REV 3, AND ERA 554153-14 REV ORIGINAL.

Part: FUEL TANK — CRACKED · airframe 76,222 hrs · 58,049 cycles

A CRACK WAS FOUND OF 1.450" ON RH CENTER TANK LOWER AFT SKIN BETWEEN STRINGER 17 AND XCW= 15.0. REPAIR IAW ER/A 554113-14AD REV. ORIGINAL.

Part: SKIN — CRACKED (LT WING) · airframe 76,222 hrs · 58,049 cycles

LEFT WING CRACK ON FIXED WING LEADING EDGE LOWER ACCESS PANEL CUT OUT STA XOS 239. PERMANENT REPAIR ON FIXED WING LEADING EDGE WAS ACCOMPLISHED PER ER/A 554133-14 REV ORIGINAL.

Part: STRINGER — CRACKED (RT WING) · airframe 76,222 hrs · 58,049 cycles

RIGHT WING CRACK ON STRINGER NR 13 STA XWC=13 RT. STRINGER 13 WAS ATTENDED WITH ER/A 554118-14 REV ORIG AND ETI-88-17-032 REV 5.

Part: SKIN — CRACKED (LT WING) · airframe 76,222 hrs · 58,049 cycles

CRACK EDGE HOLE AT LT LOWER ACCESS CUT OUT XRS= 198 AFT SIDE REF CARD 5713-2795. PERMANENT REPAIR ON CRACK WAS ACCOMPLISHED PER ER/A 554120-14AD REV ORIGINAL.

Part: STRINGER — CRACKED (RT WING) · airframe 76,222 hrs · 58,049 cycles

RIGHT WING CRACK ON STRINGER NR 13 STA XWC=13 RT. STRINGER 13 WAS ATTENDED WITH ER/A 554118-14 REV ORIG AND ETI-88-17-032 REV 5, ACCOMPLISHMENT DTE ON OR BEFORE 09-FEB-2017 WAS MONITORED WITH LOG 2891385.

Part: BEARING — CORRODED (RT MLG SUPPORT) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION AND SCRATCHES ON BEARING OF RT MLG SUPPORT FITTING. BEARING ON RT MLG SUPPORT FITTING WAS REMOVED AND NEW BEARING WAS INSTALLED PER CMM 20-10-7.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON BULKHEADS AT VENTRAL MOVABLE CEILING (WALKING BRIDGE). NEW BULKHEAD WAS FABRICATED AND REPLACED PER SRM 53-14-3 AND 51-30-2 AND AFT BULKHEAD WILL BE ATTENDED PER NRC SERIAL NR 00783.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESSORIES COMPARTMENT, CRACKED SPLICE ON STA Y=1429 BTW LONG 2R TO 3R. PERMANENT REPAIR ON SPLICE WAS ACCOMPLISHED PER ER/A 554124-14 REV ORIGINAL.

Part: BULKHEAD — CORRODED · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION BELOW AFT BULKHEAD AT VENTRAL MOVABLE CEILING. AREA WAS REPAIRED IAW SRM 53-01 FIG.4 SHEET 4.

Part: FRAME — CRACKED (BS 1510) · airframe 76,222 hrs · 58,049 cycles

CRACKED FRAME BS 1510 . THE FRAME WAS REPLACED IAW DWG 9911843 REV AC.

Part: BEAM — CRACKED (AIRSTAIR) · airframe 76,222 hrs · 58,049 cycles

CRACKED STAIRWAY TORQUE TUBE BEAM. REPLACED IAW DWG 9911992 REV AK, AND SRM 51-30-2, 51-30-5.

Part: DOUBLER — CRACKED (BS 423) · airframe 76,222 hrs · 58,049 cycles

CRACK OF 1.250 INCHES WAS FOUND ON INTERNAL DOUBLER AT BS 423, AND BETWEEN LONGERONS 27 AND 28R. REPAIRED IAW ER/A 554111-14AD REV. ORIGINAL.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESORIES BAY HAD A CRACKED SHEAR TIE BS 1380, LONGERON 15R. THE SHEAR TIE WAS REPLACED IAW SRM. 53-14-4, 51-30-5, AND 51-30-2.

Part: SUPPORT FITTING — CORRODED (RT WMLG) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON BUSHING BORE OF RT MLG SUPPORT FITTING IN REF CARD 5740-01139-4B. BUSHING BORE WAS REWORKED AND FOUND WITHIN LIMITS IAW DWG SR0957087 REV. B.

Part: FRAME — CRACKED (BS 1497) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESORIES COMPARTMENT HAD A CRACKED FRAME BS 1497 BETWEEN LONGERONS 16 & 17L. REPAIRED THE FRAME IAW SRM 53-1 FIG. 2, 51-30-2, 51-30-5, AND 51-10-3 PAR. 14, 21.

Part: INTERCOSTAL — DAMAGED (BS 1497-1510) · airframe 76,222 hrs · 58,049 cycles

CRACK AND BENT INTERCOSTAL BETWEEN BS 1497 AND 1510. THE INTERCOSTAL WAS REPLACED IAW DRAWING 9917701 REV. ORIGINAL. 51-30-2, AND 51-30-5.

Part: FITTING — DAMAGED (RT MLG) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

SCRATCHES ON RT MLG FITTING BEARING BORE. BEARING BORE WAS REWORKED AND FOUND WITHIN LIMITS PER DWG SR0957087 REV. B.

Part: FRAME — CRACKED (BS 1485) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESORIES COMPARTMENT A CRACK WAS FOUND ON THE FRAME BS 1485 . THE FRAME WAS REPAIRED IAW SRM 53-03 PAR 38.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 76,222 hrs · 58,049 cycles

AFT CARGO DOOR CRACKED ON PREVIOUS DOUBLER REPAIR. THE REPAIR WAS REPLACED IAW SRM 52-03D, FIG 8.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,222 hrs · 58,049 cycles

FLOOR PANEL FOUND DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-20-01-201.

Part: ANGLE — CRACKED (BS 1418) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESORIES BAY HAD A CRACKED ANGLE ON BS 1418 BETWEEN LONGERON 1 & 2R. THE ANGLE WAS REPLACED IAW SRM. 53-14-4 FIG. 1 (SHEET 1), 51-30-5, AND 51-10-3 PAR. 21, 14 AND 38.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON FUEL TANK ACCESS PANEL 1303C AND 1335C. THE FUEL ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR. 6, CONDITION II.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON LOWER DOOR FRAME BS 1155 - 1212 IN THE AFT CARGO. REPAIRED IAW SRM 53-05 FIG.123 SHEET 2, 51-10-3 PAR 14,21,26,38 AND 51-30-4.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,222 hrs · 58,049 cycles

CRACKED LONGERON 4L, BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG.18, 51-10-3 PAR 14,21, 51-10-4, 51-30-2, AND 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,222 hrs · 58,049 cycles

CRACKED LONGERON 4R, BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG. 18.

Part: FRAME — CRACKED (LT WING) · airframe 76,222 hrs · 58,049 cycles

LEFT WING MAIN FRAME STRINGER 11 AT XRS 160 CRACKED 2.5 INCHES. REPAIRED IAW SR09570100 REV. B.

Part: LANYARD — BROKEN (SERVICE DOOR) · airframe 76,222 hrs · 58,049 cycles

PAX CABIN, MISSING LOCK PIN AND BROKEN RELEASE LANYARD WIRE AT FWD SERVICE DOOR EVACUATION SLIDE. LOCK PIN WAS INSTALLED AND LANYARD WIRE WAS REPLACED AT FWD SERVICE DOOR EVACUATION SLIDE IN REFERENCE AMM 25-62-00.

Part: DOOR FRAME — CORRODED (AFT CARGO) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

AFT CARGO BAY HAD CORROSION ON THE LOWER DOOR FRAME FROM BS 1155 - 1212. REPAIRED IAW SRM 53-05 FIG.123 SHEET 2, 51-10-3 PAR 14,21,26,38, AND 51-30-4.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

AFT CARGO, CORROSION ON LT TIE TRACKS STA Y=1007 TO STA Y=1231 ON AFT CARGO CMPT. LT TIE TRACK STAY=1007 TO 1231 ORIG THICKNESS IS 0.060" AND SECTION CENTER EXTRUSION IS 0.100" MIN REMAINING IS 0.023" AND 0.087" RESPECTIVELY, THEREFORE ITS OUT OF LIMITS PER SRM 53-05 FIG 4C. TIE TRACK WAS REPLACED PER SRM 51-30-2, 51-30-5 AND 51-30-1.

Part: ARM — CORRODED (LT SPOILER) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

LEFT WING, PITTING CORROSION ON OUTBD FLIGHT SPOILER REACTION ARM, TORSION BAR AND CAM ARM. OUTBD FLIGHT SPOILER REACTION ARM, TORSION BAR AND CAM ARM WERE REMOVED PER AMM 27-61-06, AND NEW REACTION ARM, TORSION BAR AND CAM ARM WERE INSTALLED PER MD88 AMM 27-61-06.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESSORY COMPARTMENT, CRACKED DOUBLER ON STA Y= 1463 CAT BTW LONG 17L TO 18L. DOUBLER ON STA Y= 1463 CAT BTW LONG 17L TO 18L WAS REPAIRED PER SRM 53-01 FIG 2 (SHEET 4).

Part: FITTING — CRACKED (R1 DOOR) · airframe 76,222 hrs · 58,049 cycles

R1 DOOR, CRACKED FWD CLIP ON BEAM NR 1. CLIP WAS REPLACED PER SRM 51-30-4, 51-30-5 AND DWG 9911579 REV L.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 76,222 hrs · 58,049 cycles

PUNCTURE ON RT CUSP WEB BTW STA Y=786 AND X=-53. PUNCTURE ON CUSP WEB WAS REPAIRED PER SRM 53-01 FIG 1 SHEET 2/51-10-3 PAR 21 AND 14/51-30-5.

Part: BEAM — CRACKED (R1 DOOR) · airframe 76,222 hrs · 58,049 cycles

R1 DOOR, CRACKED BEAM NR 1 FWD END. BEAM WAS REPLACED PER SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON FUEL TANK ACCESS PANEL 1409C. THE ACCESS PANEL WAS REPLACED.

Part: SKIN — CRACKED (RT WING) · airframe 76,222 hrs · 58,049 cycles

RIGHT WING, CRACKED ON PREVIOUS REPAIR DOUBLER AT RIGHT WING LEADING EDGE XRS 253. DOUBLER WAS REPLACED IAW ER/A 490036-14 REV B.

Part: DOUBLER — DENTED (RT WING TE FLAP) · airframe 76,222 hrs · 58,049 cycles

RIGHT WING DENTED ON A PREVIOUS REPAIR DOUBLER INBD FLAP INBD GUIDE VANE. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PAR 11.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 76,222 hrs · 58,049 cycles

NR 2 CARGO DOOR HAD A CRACKED TEE AT BS 655, BEAM 1 TO LOWER EDGE AT MID CARGO DOOR. THE TEE WAS REPLACED IAW SRM 51-30-5, AND 51-30-2, AND DWG 9957664 REV N.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 76,222 hrs · 58,049 cycles

C2 DOOR HAD WEAR ON A PRODUCTION DOUBLER FWD, LOWER CORNER. THE DOUBLER WAS REPLACED IAW SRM 51-30-2 AND DWG 5910141 REV FE.

Part: SKIN — SCRATCHED (LT WING TE FLAP) · airframe 76,222 hrs · 58,049 cycles

LEFT WING :SCRATCHED ON THE LOWER FACE AT THE OTBD FLAP MID GUIDE VANE. REPAIRED IAW SRM 57-03D, PAR 11.

Part: ANGLE — CRACKED (BS 1437) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESORIES COMPARTMENT HAD A CRACKED ANGLE BS 1437 BETWEEN LONGERONS 12 & 13R. THE ANGLE WAS REPLACED IAW DWG 9911840, REV DC.

Part: CARGO TRACK — CORRODED (BS 522-788) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

MID CARGO BAY HAD CORROSION ON THE LT AND RT CARGO TRACKS BETWEEN BS 522 AND 788. THE CARGO TRACKS WERE REPLACED IAW SRM 51-10-4, 51-10-3, PAR 26, 14, AND 21, 51-30-2, 51-30-1, 51-30-5, AND 53-05 FIG 4C.

Part: ANGLE — CRACKED (BS 1437) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESORIES COMPARTMENT HAD A CRACKED ANGLE BS 1437 BETWEEN LONGERONS 12 - 13R. THE ANGLE WAS REPLACED IAW DWG 9911840, REV DC.

Part: DOUBLER — WORN (CARGO DOOR SKIN) · airframe 76,222 hrs · 58,049 cycles

WEAR ON AFT/FWD SKIN DOUBLERS AT AFT CARGO DOOR. DAMAGE ON FWD LOWER CORNER DOUBLER BLENDED OUT IAW SRM 52-01 FIGURE 1 (SHEET 3).

Part: LONGERON — CRACKED (BS 1380) · airframe 76,222 hrs · 58,049 cycles

CRACKED LONGERON 11L, BS1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG. 18.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 76,222 hrs · 58,049 cycles

CRACKED STIFFNER ON THE AFT PRESSURE BULKHEAD UNDER LONGERON END 3R. THE STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-30-2, AND 51-10-3 PAR. 14 AND 21.

Part: FRAME — CRACKED (BS 1345) · airframe 76,222 hrs · 58,049 cycles

AFT ACCESORIES COMPARTMENT HAD A CRACKED TITANIUM FRAME AT BS 1345, LONGERON 28L. THE FRAME WAS REPAIRED IAW ER/A 094719 -14 MA, REV A.

Part: BUSHING — CRACKED (HORIZONTAL STAB) · airframe 76,222 hrs · 58,049 cycles

CRACKED HINGE BUSHING ON RT OUTBOARD LUG OF HORIZONTAL STABILIZER ATTACH POINT AT VERTICAL STABILIZER REAR SPAR. NEW REPAIR BUSHINGS WERE FABRICATED PER DC-9/MD80 SRM 55-02 PAR.24(C). (LP2867305)

Part: FRAME — PUNCTURED (BS 275) · airframe 76,222 hrs · 58,049 cycles

PUNCTURE ON FRAME ANGLE AT BS 275 AND LONGERONS 17-18R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9911524. REV. N.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 76,222 hrs · 58,049 cycles

L1 DOOR HAD A CRACKED INTERCOSTAL BETWEEN BEAMS 4 AND 5. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: BEAM — CRACKED (L1 DOOR) · airframe 76,222 hrs · 58,049 cycles

L1 DOOR HAD A CRACKED BEAM NR 7 AFT END. THE BEAM WAS REPAIRED IAW SRM 52-05 PARAGRAP 74 FIG. 93.

Part: FRAME — PUNCTURED (BS 275) · airframe 76,222 hrs · 58,049 cycles

PUNCTURE ON FRAME ANGLE AT BS 275 AND LONGERONS 17-18R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-30-2, 51-3-5 AND DWG 9911524.

Part: FLOOR SUPPORT — CRACKED (BS 1287-1309) · airframe 76,222 hrs · 58,049 cycles

CRACK ON FLOOR SUPPORT BETWEEN BS 1287 - 1309, BL 0. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-1,51-30-2,51-30-5.SRM 51-10-4 AND 51-10-3 PAR 14 AND 21.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,222 hrs · 58,049 cycles

CRACKED LONGERON 16L ON BS 1437. THE LONGERON WAS REPLACED IAW SRM. 51-30-2, 51-30-5, 51-14-4, 51-10-4 AND 51-10-3 PAR. 21 AND 14.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 76,222 hrs · 58,049 cycles

DURING BHEC INSPECTION ON HORIZONTAL STABILIZER, RT UPPER REAR SPAR CAP CRACKED WAS FOUND. THE SPAR CAP WAS REPLACED DWG SR09550030 REV D AND SRM 51-30-2 AND 51-30-5.

Part: BULKHEAD WEB — CRACKED (BS 69) · airframe 76,222 hrs · 58,049 cycles

A CRACK WAS FOUND ON THE PRESSURE BULKHEAD WEB BS 69, LBL 12 . THE CRACK WAS STOP DRILLED IAW SRM 53-01 FIG.2. A DOUBLER WAS INSTALLED IAW SRM 53-01 FIG.2 SH. 3.

Part: LONGERON — CRACKED (BS 1437) · airframe 76,222 hrs · 58,049 cycles

CRACKED LONGERON 16R ON BS 1437. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5, 53-14-4, 51-10-4 AND 51-10-3 PAR. 21 AND 14.

Part: SEAT TRACK — CORRODED (BS 307-381) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON RT SEAT TRACK REPAIR PLUGS RBL 54, BS 304 AND 381. THE REPAIR PLUGS WERE REPLACED IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 547-609) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON LT REPAIR ON SEAT TRACK PLUG LBL 22, BS 547-550 AND BS 606-609. THE REPAIR PLUGS WERE REPLACED IAW SRM 53-05 FIG.4, 51-10-3 PAR. 21, 14, 38, AND 51-30-1.

Part: SEAT TRACK — CORRODED (BS 446-465) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON RT SEAT TRACK REPAIR PLUGS RBL 22 BS 446 AND 465. THE REPAIR PLUGS WERE REPLACED IAW SRM 53-05 FIG. 4.

Part: SPAR — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

VERTICAL STAB CORRODED ON THE LT & RT PLATES REAR SPAR BETWEEN HSS 150-160. THE CORROSION WAS REMOVED. UT INSPECTION WAS ACCOMPLISHED IAW SPM 04-00-07 PAR. 5 FIG. 3 SHEET 1 AND 2. FOUND TO BE WITHIN LIMITS IAW SRM 55-02 PAR. 24 FIG. 28.

Part: SEAT TRACK — CORRODED (BS 446-465) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON RT SEAT TRACK REPAIR PLUGS RBL 22, BS 446 - 465. THE REPAIRPLUGS WERE REPLACED IAW SRM 53-05 FIG. 4 AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

FWR PAX CABIN, CORROSION ON FLOOR SUPPORT FROM STA Y=237 TO Y=-256 BTW STA X=41 TO X=32. FLOOR SUPPORTS WERE REPLACE PER SRM 53-14-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 484-490) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION OUT OF LIMITS ON UPPER & LOWER RT CUSP WEB FROM BS 484 TO 490. THE RT CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG.131A-13, SRM 51-30-2, 51-30-5, SRM 51-10-3 PAR 26, 14, 21 AND 38.

Part: CUSP WEB — CORRODED (BS 565-568) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON LEFT CUSP WEB FROM BS 565 TO 568 BETWEEN LBL 54 AND 60. REPAIRED IAW SRM 53-05 FIG 131A-14.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 76,222 hrs · 58,049 cycles

DELAMINATED LEFT WING OTBD FLAP, OTBD VANE LOWER SKIN AT 9 INCH AND 38 INCH FROM INBD EDGE. REPLACED THE VANE IAW SRM 57-03D PAR.11.

Part: CUSP WEB — CORRODED (BS 835-840) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON PREVIOUS REPAIR LT CUSP WEB FROM BS 835 TO 840 BTW LBL 54 AND 60. REPLACED IAW SRM 53-05 FIG.131A-13 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 927-946) · corrosion level 2 · airframe 76,222 hrs · 58,049 cycles

CORROSION ON PREVIOUS REPAIR OF RT CUSP WEB BTW BS 927 TO 946. REPLACED IAW SRM 53-05 FIG.131A-13.

Part: PAN — CRACKED (BS 750) · airframe 76,222 hrs · 58,049 cycles

CRACK ON RING PAN LOWER AFT CORNER BS 750. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-2 AND 51-10-3 PARR. 14 AND 21.

Part: SPRING — FAILED (ELEVATOR) · airframe 75,601 hrs · 57,566 cycles

AFTER A ROUTINE APPROACH, DURING THE FLARE MANEUVER, THE CONTROL COLUMN WAS REPORTED TO MAKE AN ABRUPT MOTION IN THE FO'S HANDS. ELEVATOR AUTHORITY APPEARED TO HAVE BEEN RESTRICTED PER THE PILOT WRITE-UP. MAINTENANCE DISCOVERED THE ELEVATOR LOAD FEEL & CENTERING SPRING AT FAULT. THE SPRING WAS REPLACED WITH SATISFACTORY CHECKS PERFORMED PER MD88 AMM 27-30. THE A/C HAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · corrosion level 2 · airframe 75,452 hrs · 57,447 cycles

CORROSION WITH CRACK FS 588 AT STR 28R REF LOG 9299465. C/W PRI 550488-14, REV 0, REV 1, 334465. COMPLIED WITH ERA 550488-14, REV ORIGINAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,452 hrs · 57,447 cycles

2" CRACK LOCATED 4 FT FWD AND 3" BELOW LOWER RT CORNER OF MID CARGO DOOR. REPAIRED ON NR 001 IAW ERA 550488-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1463) · airframe 73,849 hrs · 56,319 cycles

TAIL INTERIOR - CANTED FRAME FWD WEB HAS 1" LONG CRACK FROM FASTENER HOLE NEAR WEB MIDDLE, CBS 1463, APPROXIMATELY 12" FWD & INBD OF L8L AFT END. REPAIRED BY TRIMOUT AND DOUBLER INSTALLATION. ALL WORK ACCOMPLISHED AND RECORDED ON PRI 542574-14, REV 00 AND COMPLIES WITH FINAL ERA 542574-14, REV ORIGINAL SEC I.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

RT WING UPPER SURFACE FILIFORM CORROSION ON FUEL PANEL LOCATED ON ICE DETECTION STRIPS. R & R PANEL IAW AMM 30-80-02-401.

Part: FITTING — CORRODED (GALLEY) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

GALLEY HOLD FITTING CORRODED BS 236, RBL 44. FABRICATED AND INSTALLED IAW PRI 543609-14, REV 0.

Part: SUPPORT FITTING — CORRODED (BS 223) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

GALLEY SUPPORT FITTING CORRODED BS 223, LBL 22. FABRICATED AND INSTALLED IAW PRI 543609-14, REV 0.

Part: FITTING — CORRODED (BS 215) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

GALLEY HOLD FITTING CORRODED BS 215, RBL 55. FABRICATE AND INSTALL IAW PRI 543609-14, REV. 0.

Part: FITTING — CORRODED (BS 236) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

GALLEY HOLD DOWN FITTING CORRODED, BS 236, RBL 22. FABRICATED AND INSTALLED IAW PRI 543609-14, REV 0.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

CORROSSION ON FLOOR SUPPORT BETWEEN ST 160 AND 200, RBL 6. REPLACE FLOOR SUPPORT REF SRM 51-01, PG 1, PAR 2D.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

FLOORBEAM CORRODED BS 180, RBL 8-44. REPLACED FLOORBEAM IAW SRM 53-01, FIG 1.

Part: THRESHOLD — CORRODED (L1 DOORWAY) · airframe 75,843 hrs · 57,773 cycles

CORROSION FOUND ON L1 DOOR THRESHOLD AFT END. REPAIRED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

SURFACE CORROSION ON FLOORBOARD SUPPORT BETWEEN BS 160 AND BS 200, LBL 4. R & R FLOORBOARD SUPPORT BETWEEN BS 160 AND BS 200, LBL 4. IAW SRM 51-01, PG 1, PAR 2D.

Part: FITTING — CORRODED (R1 GIRT BAR) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

R1 DOOR AFT GIRT BAR FITTING CORRODED. REPLACED FITTING IAW PRINT 3936910.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

FLOORBEAM CORRODED BS 180, RBL 8-44. REPLACED FLOORBEAM IAW SRM 53-01, FIG. 1.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

FLOORBEAM CORRODED BS 180, RBL 8-44. REPLACED FLOORBEAM IAW SRM 53-01, FIG 1.

Part: FLOOR SUPPORT — CORRODED (BS 160-180) · corrosion level 2 · airframe 73,849 hrs · 56,319 cycles

FLOOR SUPPORT CORRODED BS 160-180, RBL 44. REPLACED THE FLOOR SUPPORT IAW SRM 51-30-02.

Part: FRAME — CRACKED (BS 1485) · airframe 73,849 hrs · 56,319 cycles

TAIL INTERIOR, CANTED FRAME WEB BS 1485 HAS A TWO INCH LONG CRACK NEAR SUPPORT STRUCTURE, APPROXIMATELY 8:00 POSITION. REPAIRED BY CUTOUT AND DOUBLER INSTALLATION. ALL REPAIR WORK ACCOMPLISHED AND RECORDED ON PRI 543285-14, REV 0 AND COMPLIES WITH FINAL ERA 543285-14, REV ORIGINAL SEC I. REPAIR CLASSIFIED AS MAJOR WITH RII REQUIREMENT AND NON PSE.

Part: WEB — CRACKED (BS 1463) · airframe 73,848 hrs · 56,319 cycles

CANTED WEB, BS 1463, NEAR L7L, FWD WEB CRACKED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 71,639 hrs · 54,731 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,784 hrs · 53,464 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROWS 1-4 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,784 hrs · 53,464 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROWS 14-20 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,784 hrs · 53,464 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH THE LT AND RT OVERWING HATCHES AT ROW 25, WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,126 hrs · 52,971 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTS ABOVE SEATS 11 & 12 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,039 hrs · 52,207 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 11-15 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 66,958 hrs · 51,435 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX RECONNECTED THE LIGHT AND FUNCTIONALLY CHECKED THE SYS.

Part: RELAY — FAILED (COCKPIT) · airframe 63,603 hrs · 49,127 cycles

FLIGHT RETURNED TO DEPARTURE STATION DUE TO SMOKE AND BRIEF FLAME COMING FROM ELECTRICAL PANEL BEHIND CAPTAIN'S SEAT. CREW COMPLIED WITH QRH AND LANDED SAFELY BACK AT BWI. MAINTENANCE FOUND THE ALTERNATE HYDRAULIC PUMP CONTROL RELAY HAD FAILED. REPLACED R2-15 RELAY AND ASSOCIATED TERMINALS, THE APPROPRIATE CIRCUIT BREAKER, AND SPLICED IN NEW WIRES 1H2756A16A, 1H2756A16B, 2H2756A16A, AND 2H2756A16B FROM S3715 TO COCKPIT (TO REMOVE BURNED WIRES FOR OVERWING HEATER SYSTEM).

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,515 hrs · 49,059 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS OVER BOTH OF THE MAIN CABIN DOORS WERE INOPERATIVE. MAINTENANCE CYCLED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,602 hrs · 47,714 cycles

DURING HMV A CRACK WAS FOUND OF 2.125 INCH LENGHT ON FUSELAGE SKIN AT STA Y=1418.5 OF DORSAL FIN ATTACH AND AJOINING FUSELAGE SKIN. FUSELAGE SKIN WAS REPAIRED IAW ERA 490048-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,602 hrs · 47,714 cycles

DURING HMV LIGHTNING STRIKES WERE FOUND ON FUSELAGE SKIN BETWEEN STATIONS Y=617 AND Y=636 AT LOWER MID SECTION AND BETWEEN Y=655 AND Y=674 AT FORWARD UPPER EDGE OF THE WINDOW BELT PANEL. LT WINDOW BELT WAS REPAIRED IAW ERA 490022-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,602 hrs · 47,714 cycles

DURING HMV LIGHTNING STRIKES WERE FOUND ON FUSELAGE SKIN BETWEEN STATIONS Y=1079 AND Y=1095 AT LOWER FORWARD EDGE OF THE LT WINDOW BELT PANEL. WINDOW BELT WAS REPAIRED IAW ERA 490022-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,602 hrs · 47,714 cycles

DURING HMV TOOL MARK WAS FOUND ON AFT LOWER CORNER OF RT WINDOW FRAME STA Y=1098 TO Y=1117. WINDOW BELT WAS REPAIRED IAW ERA 490022-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV LIGHTNING STRIKES WAS FOUND ON FUSELAGE SKIN BETWEEN STATIONS: Y=788 AND Y=807 AT LOWER AFT CORNER AND LOWER FORWARD SECTION AND BETWEEN STATION Y=807 AND Y=826 AT AFT MID SECTION AND BETWEEN STATION Y=826 AND Y=845 AT LOWER MID SECTION OF THE WINDOW BELT PANEL LT WINDOW BELT STA Y=788 AND Y=807 AT LOWER AFT CORNER AND LOWER FORWARD SECTION REPAIRED IAW ERA 490045-14 REV ORG THE REST REPAIRED IAW SRM 53-05 FIG 111.

Part: SKIN — CRACKED (RT WING) · airframe 61,600 hrs · 47,713 cycles

DURING HMV A CRACK WAS FOUND ON RT WING FIXED LEADING EDGE SKIN AT RT SLAT TRACK ACCESS CUT OUT NUMBER 1289C STA XOS=284 TO XOS=289. RT WING FIXED LEADING EDGE SKIN WAS REPAIRED IAW ERA 490036-14 REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV DENTS WERE FOUND ON FUSELAGE SKIN AND REPAIR DOUBLER STA Y=208 BETWEEN LONG 19LT-20LT. FUSELAGE SKIN REPAIRED IAW ERA 488861-14 REV ORG.

Part: SKIN — WORN (RT WING) · airframe 61,600 hrs · 47,713 cycles

DURING HMV WEAR WAS FOUND ON RT WING LEADING EDGE STRUCTURE LOWER SURFACE NEAR TO FUELING CONTROL PANEL HINGE AREA STA XRS=253 AND XRS 212. RT WING LEADING EDGE LOWER SURFACE WAS REPAIRED IAW ERA 490036-14 REV A.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV A PUNCTURE WAS FOUND ON FUSELAGE SKIN SKIN STA Y=260 BETWEEN LONG 17 LT - 18 LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 12C.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV CORROSION WAS FOUND ON OUTER FUSELAGE SKIN STA Y=788 TO Y=807 BETWEEN L=28LT AND 30 BELOW RUBSTRIPS OF FILLET PANELS AREA. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53 SHEET 8 PARA 26.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV CORROSION WAS FOUND ON RT CUSP WEB STA Y=1155-1176,1212-1218 AND 1218-1231 BTW X=-54 TO X=-60 AT PAX CABIN. CUSP WEB WAS REPLACED IAW DRD 53-20-02D.

Part: BELT — SCRATCHED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV SCRATCHES WERE FOUND ON UPPER FWD CORNER OF RT WINDOW FRAME STA Y=1060 TO Y=1079. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV LIGHTNING STRIKE WERE FOUND ON FWD AND AFT UPPER CORNER ALSO FWD LOWER CORNER OF RT WINDOW FRAME STA Y=408 TO Y=427. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV TOOLING MARK WERE FOUND ON FWD LOWER CORNER OF THE RT WINDOW FRAME STA Y=522 TO Y=541. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV ORG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV CORROSION WAS FOUND ON OUTER FUSELAGE SKIN STA Y=748 TO Y= 766 AND Y=775 TO Y=793 BETWEEN L=26RT AT BELOW RUBSTRIP OF FILLET AREA

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV LIGHTNING STRIKES WERE FOUND ON FWD EDGE AND AFT UPPER CORNER OF RT WINDOW FRAME STA Y=237 TO Y=256. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV ORG.

Part: SUPPORT FITTING — DAMAGED (LT MLG) · airframe 61,600 hrs · 47,713 cycles

DURING HMV LMLD SUPPORT FITTING BEARING BORE ELONGATED. SUPPORT FITTING WAS REPAIRED IAW EA 09-093855-03AD REV B OPN 104.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV LIGHTNING STRIKES WERE FOUND ON FWD LOWER CORNER AND AFT LOWER CORNER OF RT WINDOW FRAME STA Y=275 TO Y=294. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV PRG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER RUBSTRIP OF FILLET FAIRING 2108 BETWEEN STA Y=1060-1098 AND LONG 18LT, 20LT,Y=1117-1136 AND LONG 24LT-26LT,Y=1071-1120 AND LONG 26LT-30. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV LIGHTNING STRIKES WERE FOUND ON AFT CORNER OF RT WINDOW FRAME STA Y-256 TO 275. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV ORG.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV A CRACK WAS FOUND RT CUSP WEB STA Y=1174 BTW X=-54 TO X=-60 AT PAX CABIN. CUSP WEB WAS REPLACED IAW DRD 53-20-02D.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 61,600 hrs · 47,713 cycles

DURING HMV CORROSION WAS FOUND ON RT MLG SUPPORT FITTING BUSHING BORE VERTICAL WALL. SUPPORT FITTING WAS REPAIRED IAW EA 09-093855-03AD REV B ME02.

Part: SKIN — DENTED (HORIZ STAB TAB) · airframe 61,600 hrs · 47,713 cycles

DURING HMV A DENT WAS FOUND ON UPPER SKIN OF RT GEARED TAB. GEARED TAB WAS REPAIRED IAW SRM 55-04 PAR 3A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV FOUR CRACKS WERE FOUND ON FUSELAGE SKIN AT STA Y=172,172.5,175 AND 176 OF .031" .046" .078" AND .019" LENGTH RESPECTIVELY BETWEEN LONGERON 11 AND 12 AT FORWARD UPPER CORNER DOOR JAMB (R1). FUSELAGE SKIN WAS REPAIRED IAW ERA 490024-14 REV A.

Part: BUSHING — DAMAGED (LT WING) · airframe 61,600 hrs · 47,713 cycles

DURING HMV ELONGATED BUSHING HOLES (3 EA) ON LT WING UPPER SKIN TRAILING EDGE HEATER BLANKET ATTACH POINTS. UPPER WING SKIN NR 1 AND 2 BUSHINGS WERE REPLACED AND NR 5 SKIN WAS REPAIRED IAW ERA 490384-14AD REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV TOOL MARK WERE FOUND ON AFT EDGE OF RT WINDOW FRAME STA Y=807 TO Y=826. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV ORG.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,600 hrs · 47,713 cycles

DURING HMV LIGHTNING STRIKE WERE FOUND ON AFT EDGE OF RT WINDOW FRAME STA Y=294 TO Y= 313. WINDOW BELT WAS REPAIRED IAW ERA 490019-14 REV ORG.

Part: WIRE — BROKEN (CABIN) · airframe 60,290 hrs · 46,847 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 23D TO BE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE LIGHT ASSEMBLY. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0814)(DLM88101779).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,919 hrs · 46,581 cycles

MX FOUND THE EMERGENCY TRACK LIGHTS TO BE INOPERATIVE. MX REPLACED THE BATTERIES. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — GOUGED (BS 294-313) · airframe 58,828 hrs · 45,864 cycles

GROUND DAMAGE AT STA 275 BETWEEN STR S20R AND S21R STA 294 AT LAPJOINT AND BETWEEN STR S29R AND STR 30 STA 313 BETWEEN STR S26R AND S27R ALSO DME ANTENNA SHEARED OFF. REPAIRED IAW ERA 478416-14.

Part: FRAME — CRACKED (BS 886 L18R) · airframe 55,915 hrs · 43,920 cycles

THE RT FS 886 FRAME WAS FOUND CRACKED JUST BELOW THE PASSENGER FLOOR LINE. THE FRAME WAS REPLACED PER ER/A 09-097023-14. THE REPAIR OCCURRED DURING MARCH 2005 BUT A PREVIOUS MRR RECORD COULD NOT BE FOUND.

Part: ACTUATOR — BYPASSING (T/E FLAP) · airframe 55,792 hrs · 43,829 cycles

FLAPS WOULD NOT EXTEND BEYOND 11 DEG FOR LANDING. FOUND RIGHT INBOARD FLAP ACTUATOR BYPASSING. REPLACED RT INBOARD NR 1 FLAP ACTUATOR PER AMM 27-52-02 PB 201. LEAK AND OPS CHECKS GOOD. FINAL INSTALLATION, SAFETY AND OPS CHECK GOOD PER MM 832734, DEPT 250, RII. CREW DECLARED EMERGENCY. AIRCRAFT LANDED UNEVENTFULLY.

Part: ACTUATOR — BROKEN (EMPENNAGE) · airframe 44,599 hrs · 36,111 cycles

DURING OPN 5924AD FOUND LOWER MECHANICAL STOP MAKE CONTACT WITH JACKSCREW STOP. LOWER STOP BROKE OFF. REPLACED JACKSCREW ASSEMBLY.

Part: STOP FITTING — BROKEN (HORIZ STAB) · airframe 44,599 hrs · 36,111 cycles

DURING OP 5924 AD FOUND LOWER MECHANICAL STOP MADE CONTACT WITH JACKSCREW STOP. LOWER STOP BROKEN OFF. REPLACED JACKSCREW AND STOP ASSY. ADJUSTED STABILIZER JACKSCREW CONTROL AND INDICATION PER M/M. RIG CHECKED AND OPS CKS GOOD.

Part: BALLAST — FAILED (EMERGENCY LIGHT) · airframe 43,946 hrs · 35,690 cycles

EMERGENCY PATH LIGHTS ROW 1-12 INOP. REPLACED BALLAST B5-211, OPS CHECK OK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 43,657 hrs · 35,504 cycles

ON L/O CHECK FOUND AFT SERIES OF EMERGENCY LIGHTS INOP. REPLACED BATTERY POWER SUPPLY.

Part: BOOT — TORN (RIGHT) · airframe 38,500 hrs · 31,874 cycles

ON CLIMB OUT PASSING THRU 25000 FT, GOT TAIL COMPARTMENT TEMP LIGHT. FOLLOWED THE PROCEDURES, BOTH X FEED CLOSED NO ANTI ICE. THE TEMP LIGHT WENT OUT AFTER FOUR MINUTES. _T/S FOUND RT FLOW CONTROL VALVE BOOT TORN, ALSO RT DIVERTER VALVE CLAMP LOOSE. REPLACED BOOT AND SECURED CLAMP, RAN THE ENGINES CK'S OK.

Part: CLAMP — LOOSE (TAIL COMPARTMENT) · airframe 36,147 hrs · 30,098 cycles

TAIL COMPARTMENT TEMP LIGHT CAME ON SHORTLY AFTER T/O. RAN CHECKLIST PER POM. LIGHT WENT OFF AFTER LEVEL OFF 3000 FT. LIGHT CAME BACK ON AFTER POWER INCREASED TO CLIMB. RETURNED TO MCO. RAN ENG AT T/O PWR. FOUND AUG VALVE LEAKING AT I/B CLAMP. REPLACED BOTH CLAMPS ON LT AUG VLV/RAN ENG TO T/O PWR, NO LEAKS.

Part: CONTROLLER — MALFUNCTIONED (LT PACK) · airframe 36,110 hrs · 30,072 cycles

FUMES IN COCKPIT AND CABIN WITH REDUCED POWER ON FINAL. SUSPECT ELECTRICAL OR AIR CONDITIONING, NO OTHER INDICATIONS. PER CAPTS VERBAL REPORT, CAPTAIN SMELLED FUMES FOR 3 FLIGHT LEGS AND THINKS IT IS GLYCOL (ANTI-ICE FLUID). SUSPECT LEFT PACK OVERTEMP. REPLACED LT PACK TEMP CONTROLLER, INSPECTED LT PACK PNEUMATIC DUCTING AND ACM. ACM OIL LEVEL FULL, RAN LT PACK SEVERAL HOURS, NO OVERTEMP OR SMELL NOTED. OK FOR FLIGHT.

Part: CASE — CRACKED (APU) · airframe 36,016 hrs · 29,999 cycles

ENCOUNTER ICE ON DESCENT INTO CVG. TURNED ON AIRFOIL ANTI- ICE. NOTICED SMOKY SMELL IN THE CABIN. LT PACK TRIPPED ON SHORT FINAL. PACKS TURNED OFF ON LANDING AND SMOKE WENT AWAY. FOUND APU TURBINE CASE CRACKED. REPLACED APU. UPON APU RUN, NO AIR. REPLACED SURGE VLV, AIR NOW OK. PERFORMED DUCT BURNOUT, CKS GOOD.

Part: SWITCH — MALFUNCTIONED (TAIL) · airframe 34,825 hrs · 29,114 cycles

TAIL COMP HIGH LIGHT ILLUMINATED SECONDS AFTER T/O. RETURNED AND LANDED. REPLACED HIGH TEMP SWITCHES.

Part: FCU — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENGINE FLUCTUATIONS AND EVENTUAL SHUTDOWN. RETURNED TO CVG FLT 971. ENGINE SHUT DOWN ON ITS OWN AFTER 45 SECONDS OF FLUCTUATIONS FROM CLIMB POWER TO NEAR IDLE. RAN ENGINE TO T/O AND POWER SETTINGS BELOW ALL CKS OK, NO FLUX. PERFORMED ACCELERATION CHECK. FAILED CHECK. REMOVED FUEL CONTROL AND FUEL PUMP. REINSTALLED FUEL PUMP. INSTALLED FUEL CONTROL. LEAK CK OF FUEL CONTROL AND PUMP GOOD. RAN ENGINE PER PFHB, ALL PARAMETERS CK GOOD.

Part: CLAMP — LOOSE (TAIL COMP)

TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED ON CLIMBOUT. LIGHT DID NOT EXTINGUISH UNTIL ABNORMAL PROC COMPLETED. FOUND LEFT ENGINE AUG VALVE LEAKING AT CLAMP. TIGHTENED SAME.

Part: SKIN — GOUGED (BS 570)

A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT FS 570 JUST ABOVE LONGERON 26L. THE DAMAGE WAS REPAIRED PER ERA 333518-14 AT HMV.

Part: FRAME — MISDRILLED (BS 1418)

THE FS 1418 FRAME WAS FOUND TO HAVE A DOUBLE DRILLED HOLE ATSTRINGER L1. THE DAMAGE WAS REPAIRED PER ERA 333514-14 AT HMV.

Part: SKIN — DENTED (BS 256)

A DENT WAS DISCOVERED IN THE FUSELAGE SKIN AT FS 256 BETWEEN LONGERONS 23L AND 24L. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ER/A 333520-14.

Part: STRUT — REQD SERVICE (NLG)

FLT 1407 DCA-ATL. NOSE GEAR WILL NOT RETRACT. DIVERTED INTO IAD. SERVICED STRUT.

Part: INLET — CONTAMINATED (APU)

ON CLIMBOUT, OILY SMELL OBSERVED WHILE ENGINE ANTI ICE IN USE. DISSIPATED AT ALTITUDE WHEN ANTI ICE TURNED OFF. FOUND OIL IN APU AIR INLET. CLEANED INLET, PERFORMED DUCT BURNOUT. REPLACED WATER SEPARATORS.

Part: PROXIMITY SWITCH — DIRTY (RT MLG)

RT GEAR UNSAFE LIGHT STAYED ON FOR ABOUT 30 SEC AFTER GEAR RETRACTION. LIGHT WENT OUT AND STAYED OUT AFTER THAT. CLEANED RIGHT MAIN GEAR PROX SWITCH, PROX BOX CKS GOOD.

Part: PNEUMATIC TUBE — FAILED (NR 2 ENGINE)

ON CLIMBOUT HAD NR 2 ENGINE FIRE WARNING. REDUCED POWER AND FIRE WARNING STOPPED. RETURNED TO ATL, FOUND ENGINE INLET ANTI-ICE PNEUMATIC TUBE BURST AT MID SPAN. REPLACED TUBE, OPERATION NORMAL.

Part: ANGLE — CRACKED (LT MLG WW)

OUTBD AFT MLG DOOR FRAME STRIKER CRACKED 1.50 INCH. FOUND DURING B-1 LTR CK. REPAIRED PER SRM 53-05 FIG 81A.

Part: HOSE — FAILED (TAIL COMP)

DURING CRUISE, RT HYDRAULIC SYSTEM FAILED, PRESS WENT TO ZERO. FOUND RT EDP PRESSURE LINE RUPTURED. REPLACED LINE OPERATION NORMAL.

Part: FAN — FAILED (FLIGHT DECK)

ON APPROACH TO DFW, ENCOUNTERED STRONG ACRID BURNING ODOR IN CABIN AND FLIGHT DECK. PERFORMED SMOKE AND FUME CHECKLIST, LANDED WITHOUT INCIDENT. FOUND CABIN RECIRCULATION FAN SHORTED, REPLACED FAN OPERATION NORMAL.

Part: CSD — FAILED (NR 1 ENGINE)

DURING CLIMB-OUT, THE LEFT CSD OVERHEATED. DISCONNECTED PER POM, BECAUSE RIGHT GENERATOR WAS ON MCO. RETURNED TO IAD. REPLACED CSD AND GENERATOR.