N911DA

Part: DETECTOR — MISSING (NLG) · airframe 61,139 hrs · 33,571 cycles

BOTH NOSE LANDING GEAR DEBRIS DEFLECTORS ARE MISSING. BOTH NOSE GEAR DERIS DEFLECTOR CARRIED OVER TO CDL 32-37-01. REMOVED AND REPLACED RH NLG DEBRIS DEFLECTOR PER MD90 AMM32-37. LH DEBRIS DEFLECTOR DID NOT MAKE FLIGHT TO PHL. REF LOG # 4865714 FOR NEW CDL OF FL DEBRIS DEFLECTOR. REMOVED CDL PLACARD. (LP#4018268)

Part: FLOOR SUPPORT — CORRODED (BS 190) · corrosion level 2 · airframe 60,950 hrs · 33,445 cycles

STA 190 L/H SIDE JUST INSIDE L1 DOOR FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT ANGLE. REFERENCE MD90 SRM 53-10-01 VOLUME III. (LP# 0813773)

Part: WEB — DAMAGED (VERTICAL STAB) · airframe 59,320 hrs · 32,435 cycles

VERTICAL STAB WEB AT STA YV 157.7 LEFT SIDE NEAR STAB SCREWJACK HAS DAMAGE. REPAIR PER ERA 566268-14 REV ORG.

Part: CHANNEL — CRACKED (VERTICAL STAB) · airframe 59,320 hrs · 32,435 cycles

CHANNEL CRACKED AROUND JACKSCREW.

Part: FLOORBOARD — DELAMINATED (FWD GALLEY) · airframe 59,320 hrs · 32,435 cycles

DELAMINATED FLOORBOARD IN THE FORWARD GALLEY. A NEW FLOORBOARD WAS INSTALLED DURING C-CHECK ON N/R 302.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 57,794 hrs · 31,509 cycles

EXIT SIGN MISSING ABOVE L2 DOOR. FOUND WIRE L982214 OFF T-STRIP. INSTALLED EXIT SIGN IAW DWG 5963985-1. OPERATION CHECKS GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,329 hrs · 31,278 cycles

L1 AND R1 DOOR EMERGENCY EXIT ARROW LIGHTS INOPERATIVE. REMOVED AND REPLACED FUSES. OPERATION CHECKED GOOD.

Part: ACCESS PANEL — CRACKED (WING) · airframe 57,701 hrs · 31,461 cycles

CRACK ON OUTBOARD FORWARD CORNER OF FUELING PANEL. REPAIRED IAW PRI/ERA 559426-14.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 56,643 hrs · 30,920 cycles

LEFT VERTICAL STABILIZER FOUND SECOND HOLE FROM BOTTOM DAMAGED. REPAIRED IAW ERA 554885-14D.

Part: SPRING — OUT OF POSITION (TAILCONE) · airframe 56,643 hrs · 30,920 cycles

TAIL CONE LEFT UPPER LOCKING SPADE HAS SPRING OUR OF POSITION. REPOSITIONED SPRING IAW MM.

Part: CABLE — OUT OF POSITION (TAILCONE) · airframe 56,635 hrs · 30,916 cycles

TAIL CONE CABLE TOO CLOSE TO CONDUIT. ADJUSTED CONDUIT IAW MM.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 54,091 hrs · 29,407 cycles

VERTICAL STABILIZER L/E FORWARD TIP HAS CRACK THRU FASTENER HOLE APPROXIMATELY, BS 1460. REPAIRED IAW SRM 55-30-05, FIG 19.

Part: OIL SYSTEM — LEAKING (ENGINE) · airframe 54,031 hrs · 29,367 cycles

UPON ENGINE SHUTDOWN, GROUND CREW REPORTED EXCESSIVE SMOKE COMING FROM NR 1 ENGINE TAIL PIPE. MAINTENANCE TROUBLESHOT. FOUND TURBINE EXHAUST BLADES WET WITH OIL. OIL BEGINNING TO POOL. IAW PROPULSION ENGINEERING CHANGE NR 1 OIL QUANTITY TRANSMITTER AND NR 4 BEARING SCAVENGE VALVE. LEAK AND OPERATION CHECKS OK.

Part: FRAME — CORRODED (BS 1344) · airframe 54,116 hrs · 29,420 cycles

FRAME CORRODED AT BS 1344, LONGERON 28R. REPAIRED IAW SRM 53-10-02, FIG 2.

Part: SPAR — CRACKED (LT WING) · airframe 54,016 hrs · 29,358 cycles

UPPER DIAMOND DOUBLER CRACKED ON OTBD EDGE AT REAR SPAR, LT WING. REPAIRED CRACK IAW SRM 51-10-03, FIG 3 AND PRI 543919-14, REV O.

Part: BOTTLE — LOW (DOOR SLIDE) · airframe 54,031 hrs · 29,367 cycles

L1 DOOR SLIDE PRESSURE LOW. R & R SLIDE.

Part: SKIN — CRACKED (BS 1531) · airframe 54,016 hrs · 29,357 cycles

AIRCRAFT SKIN HAS 2.75" LONG CRACKS AT ADJACENT RIVETS IN CANTED FRAME AT BS 1531, OTBD OF AIRSTAIR CUTOUT, LT EDGE.

Part: BULKHEAD — DAMAGED · airframe 54,016 hrs · 29,357 cycles

APB, 2 FASTENERS FOUND ON APB SPLICE LOWER SIDE BETWEEN L26L AND L27L. REPAIRED IAW ERA 543286-14, REV O.

Part: BULKHEAD — DAMAGED · airframe 54,016 hrs · 29,357 cycles

APB 2 FASTENERS FOUND ON APB SPLICE LOWER SIDE BETWEEN L26R AND L27R. REPAIRED IAW ERA 543286-14, REV O.

Part: LONGERON SPLICE — CORRODED (BS 1328-1344) · airframe 54,016 hrs · 29,357 cycles

BS 1328-1344, LONGERON SPLICE AT 29R CORRODED. FABRICATED SPLICE IAW SRM 53-10-01, FIG 7.

Part: LONGERON — CORRODED (BS 1355-1366) · airframe 54,016 hrs · 29,357 cycles

BS 1355-1366, LONGERON 27R CORRODED. REPAIRED IAW SRM 53-10-01.

Part: SKIN — CORRODED (BS 1328-1344) · airframe 54,016 hrs · 29,357 cycles

EXTERIOR SKIN PILLOWED AT BS 1328-1344, LONGERON 29R. REPAIRED IAW SRM 53-31-04, FIG 4.

Part: LONGERON — CORRODED (BS 1344-1366) · airframe 54,016 hrs · 29,357 cycles

LONGERON, BS 1344-1366, L28R CORRODED. REPAIRED IAW SRM 53-10-01, PARA 6.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 53,860 hrs · 29,260 cycles

CRACK FOUND AT RT MLG WHEEL WELL OPENING FORWARD JAMB. INSTALLED NEW DOOR JAMB IAW ERA 542843-14, REV 1. CHECKS OK.

Part: SLIDE — NO TEST (L1 DOOR) · airframe 51,558 hrs · 27,877 cycles

L1 DOOR FAILED DOOR SLIDE DEPLOYMENT, SYSTEM OPS CHECK FORECAST 92-0525-8-0006. LP 1853787.

Part: LIGHT — SPARKS (CABIN) · airframe 50,397 hrs · 27,112 cycles

FLIGHT CREW REPORTED THAT SIDEWALL LIGHTS AT ROW 32A WERE SPARKING. MAINTENANCE R & R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CORRODED (BS 826-845) · airframe 49,042 hrs · 26,283 cycles

FUSELAGE EXTERIOR SKIN BETWEEN FS 826-845, LONGERON 28-29R HAS CORROSION UNDER RUBSTRIP. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW ERA 520314-14, REV O.

Part: PAN — CORRODED (BS 200-215) · airframe 49,041 hrs · 26,282 cycles

FORWARD CABIN FLOOR FOUND CORROSION ON FLOOR PAN, BS 200-215, RBL 15-25. CUTOUT DAMAGE. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 51-10-03, 51-30-05, AND 51-30-02.

Part: FRAME — CORRODED (BS 1364) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON FRAME DOUBLER BS 1364, L29L. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-02, 51-30-02, AND 51-3-10-05.

Part: FRAME — CORRODED (BS 1364) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON FRAME DOUBLER, BS 1364, L29L, CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-05, 51-10-03, 53-10-02.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 49,041 hrs · 26,282 cycles

AFT CARGO DOOR FRAME BEAM CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED DOOR FRAME BEAM IAW SRM 51-30-05, 51-30-02 AND DWG 5936038.

Part: SKIN — CORRODED (BS 953) · airframe 49,041 hrs · 26,282 cycles

CENTER WING UPPER EXTERNAL SKIN, BS 953 XCW 58.6 RIGHT HAS CORROSION. REMOVED CORROSION. ALODINED, FLAP PEENED REWORKED AREA IAW ERA 520317-14, REV 1.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 49,041 hrs · 26,282 cycles

MID CARGO DOOR FRAME BEAM CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW DOUBLER AND SPACER IAW SRM 53-60-02.

Part: STIFFENER — DEBONDED (CABIN FLOOR) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN LEFT FORWARD OTBD FLOOR PANEL HAS A DEBONDED STIFFNER. REPAIRED STIFFNER IAW ERA 417243-14MA.

Part: LONGERON — CORRODED (BS 1379-1395) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON LONGERON 27R BETWEEN BS 1379-1395. CUT OUT DAMAGED SECTION. FABRICATED NEW LONGERON SECTION IAW SRM 53-10-01, 41-30-05, AND 51-30-02.

Part: LONGERON — CORRODED · airframe 49,041 hrs · 26,282 cycles

CORROSION ON LONGERON 28R JUST FORWARD OF TIE. CUT OUT DAMAGE. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 53-10-01, 51-10-03 AND 53-10-01.

Part: WEB — CORRODED (BS 180-200) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN BETWEEN, BS 180-200, RBL 10-43 WEB CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 51-10-01, 51-10-05, & 51-30-02.

Part: LONGERON — CORRODED (BS 1379-1395) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON LONGERON 29R, BETWEEN BS 1379-1395, REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 51-30-02, 51-10-05 AND 53-10-01, PARA 4, FIG 7.

Part: LONGERON CLIP — CORRODED (BS 1393) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON LONGERON TIE, BS 1393, L29R. R & R LONGERON TIE IAW SRM 51-30-05 AND DWG 5936667, REV WB.

Part: LONGERON — CORRODED (BS 1393) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON LONGERON 28R, BS 1393. R & R LONGERON IAW SRM 51-30-05 AND DWG 5936667.

Part: LONGERON SPLICE — CORRODED (BS 1328-1344) · airframe 49,042 hrs · 26,283 cycles

CORROSION ON LONGERON SPLICE 29R BETWEEN BS 1328 AND 1344. REMOVED LONGERON SPLICE. FABRICATED AND INSTALLED NEW LONGERON SPLICE IAW SRM 53-10-01, 51-10-03 AND 51-01-00.

Part: LONGERON CLIP — CORRODED (BS 1395) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON LONGERON TIE, L27R, BS 1395. R & R LONGERON TIE IAW SRM 51-30-05 AND DWG 5936667.

Part: FRAME — CORRODED (BS 1345) · airframe 49,042 hrs · 26,283 cycles

CORROSION ON FRAME BS 1345 BETWEEN L26-27R BOTH SIDES, TASK 53-100-16. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME IAW SRM 53-10-02.

Part: SEAT TRACK — DAMAGED (BS 579-646) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN SEAT TRACK GOUGED AND SCRATCHED AT BS 579-646, RBL 22. BLENDED OUT GOUGES. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: DOUBLER — CORRODED (BULKHEAD) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON AFT SIDE OF BULKHEAD ON THE STRAP, JUST FORWARD OF APB, BL 11L - 11R. R & R DOUBLER IAW SRM 51-10-05, RIG 1 AND DWG 9915561.

Part: FRAME — CORRODED (BS 1344) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON FRAME, BS 1344, L29L-29R. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED AND INSTALLED ANGLE IAW SRM 53-10-02, 51-10-03 AND 51-30-05.

Part: FORMER — CORRODED (BS 1307) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON FORMER, BS 1307, BETWEEN L28-29R. CUT OUT DAMAGE. FABRICATED AND INSTALLED FORMER SECTION IAW SRM 53-10-02, FIG 3.

Part: SEAT TRACK — CORRODED (BS 864-1079) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN SEAT TRACK BETWEEN FS 864-1079+10 CORRODED AND GOUGED AT MULTIPLE LOCATIONS, RBL 54. R & R SEAT TRACK FROM BS 856-1144, IAW SRM 53-40-01, FIG 6 AND 51-30-01.

Part: SUPPORT — CORRODED (BS 1269-1276) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON SUPPORT BS 1269-1276 BETWEEN L29-30R,. R & R SUPPORT IAW DWG 5936071.

Part: SUPPORT — CORRODED (BS 1269-1276) · airframe 49,041 hrs · 26,282 cycles

CORROSION ON FRAME SUPPORT BS 1269-1276 BETWEEN L29-30R, R & R FRAME SUPPORT IAW DWG 5936021.

Part: CUSP WEB — CRACKED (BS 1248) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, LT SIDE CUSP WEB, BS 1248, CRACKED. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-30-02, 51-10-05, 51-10-03 AND 51-10-00.

Part: CUSP WEB — CRACKED (BS 593) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, LT SIDE CUSP WEB, BS 593, CRACKED. R & R CUSP WEB IAW DWG 9910151.

Part: SEAT TRACK — DAMAGED (BS 1260-1364) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN SEAT TRACK, LBL 22, BS 1260-1364 HAS NUMEROUS LOCATIONS OF GOUGES AND CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, FIG 4, 51-30-01, AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RT SIDE CUSP WEB, BETWEEN BS 541-560 CORRODED. FOUND 100 PERCENT MATERIAL LOSS. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-20-02, FIG 19.

Part: CUSP WEB — CORRODED (BS 731-750) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RT SIDE CUSP WEB BETWEEN BS 731-750 CORRODED. CUT OUT DAMAGED AREA. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SPLICE REPAIR AND CUSP WEB IAW SRM 53-20-02, FIG 26.

Part: CUSP WEB — CORRODED (BS 962-1003) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RT CUSP WEB, RBL 57, BS 962-1003 CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED CUSP WEB IAW SRM 51-30-02.

Part: CUSP WEB — CORRODED (BS 902-962) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN RT CUSP WEB, RBL 57, BS 902-962 CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-10-03 AND DWG 9940443.

Part: CUSP WEB — CORRODED (BS 522-541) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RT SIDE CUSP WEB, BS 522-541 CORRODED. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 750-757) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RIGHT SIDE CUSP WEB, BETWEEN BS 750-757 CORRODED. 100 PERCENT MATERIAL LOSS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 49,041 hrs · 26,282 cycles

CUSP WEB, BS 560-579 CORRODED. FOUND CORROSION OUT OF LIMITS. REMOVED CUSP WEB, FABRICATED AND INSTALLED DOUBLER REPAIR AND FILLER IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 769-775) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, LEFT CUSP WEB, BETWEEN BS 769 - 775 IS CORRODED. REPAIRED MAIN CABIN CUSP WEB IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RIGHT CUSP WEB BETWEEN BS 655-674 IS CORRODED. REMOVED CUSP WEB AND FABRICATED NEW CUSP WEB IAW SRM 53-10-03 AND SRM 51-10-05.

Part: CUSP WEB — CORRODED (BS 653) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RIGHT CUSP WEB , BS 653 CORRODED. REMOVED CUSP WEB AND FABRICATED NEW CUSP WEB IAW SRM 53-10-02 AND SRM 51-10-05. INSTALLED IAW SRM 51-10-03.

Part: CUSP WEB — CORRODED (BS 674-685) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, RT CUSP WEB, BS 674-685 CORRODED. REMOVED CORROSION AND FOUND 100 PERCENT MATERIAL LOSS. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 49,041 hrs · 26,282 cycles

MAIN CABIN, LEFT SIDE CUSP WEB, BETWEEN BS 541-560 CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 51-30-02.

Part: INTERCOSTAL — CORRODED (BS 1364-1379) · airframe 47,268 hrs · 25,206 cycles

INTERCOSTAL AT L26R BETWEEN BS 1364 AND 1379 CORRODED. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL IAW SRM 51-30.

Part: LONGERON — CORRODED (BS 1469-1486) · airframe 47,286 hrs · 25,219 cycles

FOUND CORROSION ON LONGERON 27R BETWEEN STA 1469 AND 1486.

Part: ANGLE — CRACKED (BS 1475 L2R) · airframe 46,398 hrs · 24,745 cycles

BS 1475 LONGERON 2R, FRAME TO LONGERON ANGLE CRACKED. INSTALLED ANGLE IAW ER/A 510524-14, REV O, STEP 2.

Part: BRACKET — CRACKED (BS 1475) · airframe 46,398 hrs · 24,745 cycles

BS 1475 LONGERON 2R CRACK IN BRACKET FOR DUCT SUPPORT ROD 3 INCHES DOWN FROM LONGERON 2R (AFT SIDE OF FRAME). FABRICATED NEW BRACKET IAW DWG 5911432 TREATED AND PRIMED. INSTALLED BRACKET IAW DWG 5911432.

Part: ANGLE — CRACKED (BS 1475 L2R) · airframe 46,398 hrs · 24,745 cycles

IAW ERA 488912-14, REV B, REV 01, STEP NR4 1475 LONGERON 2R 7" SUPPORT ANGLE JUST FORWARD OF FRAME AT LONGERON HAS 2 CRACKS IN ANGLE. MATCH DRILLED AND DEBURRED NEW ANGLE. INSTALLED ANGLE IAW DWG SG90530003.

Part: SKIN — CRACKED (BS 1475) · airframe 46,398 hrs · 24,745 cycles

FOUND RIVET HAD POPPED AND SKIN APPEARS CRACKED AT STA 1475 BETWEEN L2R AND L3R. DRILLED OUT RIVET AND BLENDED PAINT. ACCOMPLISHED HVEC AROUND RIVET IAW NDT SRM 06-10-01. CRACK INDICATIONS ON FORWARD AND AFT SIDES OF RIVET. REPAIRED CRACK IN FUSELAGE SKIN IAW ERA 510524-14 AND DWG SG90530003.

Part: SKIN — CRACKED (BS 1475 L2-3R) · airframe 46,398 hrs · 24,745 cycles

BS 1475 L2 -3R SKIN CRACKED. SECTION I OF ER/A 510524-14 ISSUED FOR CRACK REPAIR.

Part: LONGERON — DAMAGED (BS 1495) · airframe 46,398 hrs · 24,745 cycles

BS 1495, LONGERON 4R CRACKED. REMOVED DAMAGED LONGERON FROM BS 1488 - 1501. PERFORMED HFEC, NO FINDINGS, DAMAGE CONTAINED. FABRICATED NEW SECTION OF LONGERON IAW DWG 5910288. FOUND NEW SPLICE PIECE FOR AFT CUT POINT BS 1501 IAW DWG 3924814-501 AND SRM 53-10-01, FIG 7. TREATED AND PRIMED REPAIR SECTION OF LONGERON AND REPAIR SPLICE. INSTALLED IAW SRM 53-10-01.

Part: LONGERON — DAMAGED (BS 1495) · airframe 46,398 hrs · 24,745 cycles

BS 1495 LONGERON 3R CRACKED. REMOVED DAMAGED LONGERON FROM BS 1488 - 1501. ACCOMPLISHED HFEC ON LONGERON IAW NDT SPM 06-10-01.001. NO FINDINGS. DAMAGE CONTAINED. FABRICATE A NEW SECTION OF LONGERON IAW DWG 5910228. FORMED NEW SPLICE PIECES FOR AFT CUT POINT AT BS 1501 IAW DWG 3924814-501. TREATED AND PRIMED REPAIR SPLICE AND LONGERON SECTION. INSTALLED LONGERON 3R IAW SRM 53-10-01, FIG 7 AND DWG 5910228.

Part: LONGERON — CRACKED (BS 1475 L2R) · airframe 46,398 hrs · 24,745 cycles

BS 1475, LONGERON 2R HAS TWO CRACKS ON AFT END. REMOVED DAMAGED LONGERON BS 1463 - 1478. ACCOMPLISHED HFEC ON LONGERON IAW NDT SPM 06-10-01 .001. NO FINDINGS, DAMAGE CONTAINED. OK TO INSTALL. INSTALLED LONGERON 2R IAW ERA 510524-14 REV O, STEP 20.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,868 hrs · 24,453 cycles

MULTIPLE BULBS INOPERATIVE, FWD RT OVERWING EXIT EMERGENCY LIGHT. LAMPED AND OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 45,154 hrs · 24,013 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. FOUND SEVERAL LIGHT ASSEMBLIES DISCONNECTED. RECONNECTED AND RELAMPED AS REQUIRED. OPERATION CHECKS GOOD.

Part: LANYARD — DISCONNECTED (R1 DOOR SLIDE) · airframe 45,154 hrs · 24,013 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND R1 DOOR LANYARD OUT OF SLIDE. REINSTALLED LANYARD. AIRCRAFT OKAY FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,442 hrs · 23,628 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND 1L FLIGHT ATTENDANT EMERGENCY EXIT SIGN HAS FOUR BULBS OUT. RELAMPED OPERATION CHECKS GOOD.

Part: LIGHT — INOPERATIVE (TAILCONE) · airframe 44,442 hrs · 23,628 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAIL CONE DEPLOY HANDLE EMERGENCY EXIT LIGHT HAS TWO BULBS INOPERATIVE. RELAMPED ALL FIVE BULBS L2-873. OPERATION CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 44,442 hrs · 23,628 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND L1 DOOR VERTICAL EMERGENCY EXIT SIGN HAS TWO BULBS INOPERATIVE. RELAMPED. OPERATION CHECKS GOOD.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 41,695 hrs · 22,268 cycles

FLIGHT DIVERTED INTO SLC DUE TO AN ELECTRICAL ODOR EMANATING FROM THE RIGHT AFT LAVATORY. MAINTENANCE TROUBLESHOT PER MANUAL. RAN PACKS USING ENGINE AND APU AIR. NO ODOR COMING FROM AIR CONDITIONING OUTLETS. FOUND OVERHEATED CEILING LIGHT BALLAST AT ROW 37 AND DIMMER CONTROL FUSES BLOWN. REMOVED AND REPLACED FUSES AND BALLAST. ALL OPERATION CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,634 hrs · 22,242 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY EXIT OVER WING FORWARD LEFT SIDEWALL INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR FORWARD LEFT & RIGHT OVERWING EXIT EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-03. OPERATION OF LIGHT NOW CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,634 hrs · 22,242 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY EXIT OVERWING FORWARD RIGHT SIDEWALL INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR FORWARD LEFT & RIGHT OVERWING EXIT EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-03. OPERATION OF LIGHT NOW CHECKS NORMAL.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 41,634 hrs · 22,242 cycles

DURING LIGHT TEST FIRST CLASS CEILING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE TROUBLESHOT AND FOUND BATTERY PACK B5-236 WITH BLOWN FUSE. BATTERY PACK AND EXIT SIGN WAS REPLACED. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: LIGHT — MALFUNCTIONED (GALLEY) · airframe 41,479 hrs · 22,181 cycles

FLIGHT CREW REPORTED ELECTRICAL ODOR EMANATING FROM FORWARD RIGHT GALLEY. THE OVENS WERE OFF SO THE GALLEY POWER WAS THEN TURNED OFF. THE ODOR DISSIPATED SHORTLY THEREAFTER SO THE GALLEY POWER REMAINED OFF FOR REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED GALLEY G2 AND FOUND ELECTRICAL ODOR COMING FROM THE WORK LIGHT AND RE-LAMPED IT. OPERATIONAL CHECKS WERE GOOD SO THE AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 1494 S2L) · airframe 41,167 hrs · 22,051 cycles

FUSELAGE SKIN CRACKED AT STA 1494 FOUND ON OVERWEIGHT LANDING INSP. ACCOMPLISHED REPAIR IAW ER/A 488962-14, REV O.

Part: SKIN — CRACKED (BS 1475) · airframe 41,167 hrs · 22,051 cycles

FUSELAGE SKIN CRACKED, FOUND ON HARD LANDING INSP. ACCOMPLISHED MAJOR SKIN CRACK REPAIR AT STA 1475 BETWEEN L-2L &L-3L IAW ER/A 488912-14, REV O.

Part: MOUNT — CORRODED (ENGINE) · airframe 36,229 hrs · 19,460 cycles

ENGINE AFT MOUNT SUPPORT FITTING FASTENERS CORRODED. REPAIRED IAW 02-469466-12 ME01 AND ME02.

Part: RELAY — SHORTED (MASTER BATTERY) · airframe 38,164 hrs · 20,580 cycles

AFTER BLOCK IN IRS NR 1 BATTERY FAIL LIGHT ILLUMIN W/ ASSOCIATED CAUTION MSG APU DID NOT ST AND BATTERY VOLT READ 10 VOLTS ALSO NOTED ACRID ELECTRICAL ODOR IN COCKPIT AND FIRST CLASS CABIN. REPLACED BATTERY CHARGER BATTERY CHARGER RELAY R2-56 AND 3 SHIPS BATTERIES. NO HELP FOUND APU START RELAY SHORTED REPLACED SAME BATTERY CHARGE OPS CHECK NORMAL APU STARTS NORMAL ALSO REPLACED LT AND CTR BATTERY CONNECTOR.

Part: ENGINE — DIRTY (NR 1) · airframe 37,207 hrs · 20,014 cycles

DESCENT AT 15000 TO LEVEL OFF POWER INCREASE GOT STATUS MSG LT STATOR VANE FAIL THEN CREW NOTIFICATION OF LOUD POPPING NOISES ON LEFT AFT SIDE, THEN LEFT ENGINE RPM DECREASED TO 35 PCT N1 AND EGT NEAR 600C. OIL PRESS AT 85 PSI. SHUTDOWN WAS 620C NO OTHER ABNORMAL ENG VIBRATION INDICATIONS. EXAMINED INLET EXHAUST AND BLEED VLVS. NO FOREIGN MATERIAL. ACCOMPLISHED BOROSCOPE OF 3 AND 6 STAGES - NO ITEMS. REPLACED VSV ACTUATOR PER MM, RAN GAT TEST-PASSED. REPLACED EEC, CHECKS GOOD POWER ASSURANCE CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 37,207 hrs · 20,014 cycles

DESCENT AT 15000 FT TO LEVEL OFF POWER INCREASE GOT STATUS MSG "L" STATOR VANE FAIL. THEN CREW NOTIFICATION OF LOAD POPPING NOISES ON LEFT AFT SIDE, THE LEFT ENGINE RPM DECREASED TO ~35% N1 AND EGT NEAR 600C. OIL PRESS AT 85 PSI. SHUT DOWN ENGINE AS EGT STARTED TO INCREASE MAX EGT SEEN BEFORE SHUT DOWN WAS 620C. NO OTHER ABNORMAL ENG VIBRATION INDICATIONS. PERFORMED BOROSCOPE - NO DEFECTS NOTED. REPLACED VSV ACTUATOR PER MM. RAN GAT TE________________________________________ GOOD. REPLACED EEC.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 33,888 hrs · 18,071 cycles

HORZ STAB PIVOT BEARING LUGS (4 EA) AND BARE SLEEVES (2 EA) CORRODED AND PITTED. INSTALLED REPAIRED HORZ STAB LUGS, IAW DELTA ER/A 466670-14 REV. DATE 19FEB08 I/R.

Part: SKIN — CHAFED (BS 160) · airframe 33,888 hrs · 18,071 cycles

DURING HMV AT OKC, THE AIRCRAFT SKIN AT THE FWD LOWER CORNER OF THE PASSENGER DOOR AIRSTAIR CUTOUT WAS FOUND CHAFED. THE CHAFED AREA WAS INSPECTED AND TREATED PER BOEING INSTRUCTIONS.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 33,888 hrs · 18,071 cycles

DURING ACCOMPLISHMENT OF SKIN PANEL SPLICE REPAIR PER SR09550000, TWO HOLES HAD SHORT EDGE DISTANCE CONDITION. A/C WAS AT HMV OKC AAR, WHO CONTACTED BOEING FOR APPROVAL OF CONDITION. SUBJECT CONDITION IS DOCUMENTED ON ERA 466169-14.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 33,888 hrs · 18,071 cycles

DURING CURRENT HMV, CORROSION WAS FOUND IN THE HORIZONTAL STABILILZER CENTER SECTION HINGE BORES, BOTH LT AND RT. SUBJECT CORROSION WAS REMOVED BY SPOTFACING AND OVERSIZING THE BORES BEYOND THE SRM ALLOWABLE LIMITS. AS SUCH, BOEING WAS CONTACTED FOR APPROVAL OF REPAIR, AND IS DOCUMENTED IN ER/A 466670-14.

Part: SHEAR TIE — CORRODED (BS 1344) · airframe 33,888 hrs · 18,071 cycles

AFT CARGO BAY SHEAR TIE AFT SIDE OF STA 1344 BETWEEN LONGERON 27L AND 26R CORRODED. REMOVED AND REPLACED DAMAGED SHEAR TIE WITH FABRICATED PARTS IAW DAC DWG 9957739 AND MD90 SRM 51-30-02.

Part: FRAME — CRACKED (BS 1019) · airframe 33,888 hrs · 18,071 cycles

RIGHT MLG BAY FORWARD FRAME CRACKED APPROXIMATELY FS 1019 RBL 56.5. REMOVED AND REPLACED RIGHT MLG BAY FORWARD FRAME, IAW MD90 SRM 51-30-02, 51-30-05 AND 51-10-03.

Part: STRAP — CORRODED (BS 1364 S29LR) · airframe 33,888 hrs · 18,071 cycles

AFT CARGO BAY TIE STRAP ATTACHED TO TOP SIDE OF LONG 29R, 30, AND 29L STA 1364 CORRODED. REMOVED AND REPLACED AFT CARGO TIE STRAP, IAW MD90 SRM 51-30-02.

Part: LONGERON — CORRODED (BS 1344-1364) · airframe 33,888 hrs · 18,071 cycles

AFT CARGO BAY LONGERON 29L BETWEEN STA.1344 AND 1364 CORRODED. REMOVED AND REPLACED CORRODED LONGERON SECTION, IAW MD90 SRM 51-30-02, 51-30-05 AND 53-10-01 FIG 7.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 33,888 hrs · 18,071 cycles

CORROSION ON LWR LEG OF MID CARGO DOOR BEAM IN NUMEROUS PLACES ENTIRE LENGTH. REPAIRED DOOR BEAM, IAW MD80 SRM 53-05D FIG 63.

Part: FRAME — CHAFED (BS 1003) · airframe 33,888 hrs · 18,071 cycles

LEFT MAIN LANDING GEAR BAY FORWARD FRAME CHAFED FS 1003 LBL36. REMOVED AND REPLACED INBOARD FORWARD FRAME, IAW MD90 SRM 51-30-02 AND 51-30-05.

Part: SHEAR TIE — CRACKED (BS 1486) · airframe 33,888 hrs · 18,071 cycles

AFT ACCESSORY COMPARTMENT STATION 1486 LEFT OF LONGERON 1 SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE, IAW MD90 SRM 51-10-05 AND 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,888 hrs · 18,071 cycles

AFT OF LEFT HYDRAULIC SERVICE BOX SUPPORT IS CRACKED. REMOVED AND REPLACED OUTBOARD FRAME, IAW MD90 SRM 51-30-02 AND 51-30-05.

Part: LONGERON — CORRODED (BS 1344-1364 L29) · airframe 33,888 hrs · 18,071 cycles

AFT CARGO BAY LONGERON 29R BETWEEN STA 1344 AND 1364 CORRODED. REMOVED AND REPLACED CORRODED LONGERON SECTION, IAW MD90 SRM 51-30-01, 51-30-05 AND 53-10-01 FIG 7.

Part: PAN — CORRODED (CARGO BAY) · airframe 33,888 hrs · 18,071 cycles

2 AREAS OF CORROSION AT RIVNUTS ON LWR PORTION OF FWD CARGO DOOR JAMB AT MIDDLE AND AFT END. REPAIRED CARGO DOOR JAMB, IAW MD80 SRM 53-08D FIG 44.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 33,888 hrs · 18,071 cycles

AFT CARGO BAY BRACKET AT AFT END OF LWR BEAM (DOOR CUT-OUT) CORRODED. REMOVED AND REPLACED BRACKET IN AFT OF LWR BEAM, IAW MD90 SRM 51-30-05.

Part: BRACKET — CORRODED (CARGO DOORWAY) · airframe 33,888 hrs · 18,071 cycles

AFT CARGO BAY BRACKET AT FWD END OF LWR BEAM (DOOR CUT OUT) CORRODED. REMOVED AND REPLACED BRACKET IN AFT CARGO BAY AT FWD END OF LWR BEAM, IAW MD90 SRM 51-30-05.

Part: BRACKET — CORRODED (CARGO DOORWAY) · airframe 33,888 hrs · 18,071 cycles

AFT CARGO BAY BRACKET AT LWR END OF CARGO DOOR AFT CUT-OUT CORRODED. REMOVED AND REPLACED AFT CARGO BAY BRACKET AFT LWR END OF CARGO DOOR CUT-OUT, IAW MD90 SRM 51-30-05.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 33,888 hrs · 18,071 cycles

RT INBOARD VERTICAL STAB LUG CORRODED. REPAIRED RT INBOARD VERTICAL STAB LUG, IAW DAL ER/A 466168-14 DATED 02/15/08 REV A.

Part: LUG — CORRODED (VERT STAB) · airframe 33,888 hrs · 18,071 cycles

RT O/B VERT STAB LUG CORRODED. RT O/B VERT STAB LUG REPAIRED, IAW DAL ER/A 466168-14 DATE 02/15/08 REV A.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 33,888 hrs · 18,071 cycles

LT O/B VERTICAL STABILIZER LUG CORRODED. REPAIRED LEFT OUTBOARD VERTICAL LUG (STAB), IAW MD90 SRM 55-30-05.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 33,888 hrs · 18,071 cycles

LT INBOARD VERTICAL STABILIZER LUG CORRODED. REPAIRED LT INBOARD VERTICAL STAB LUG, IAW MD90 SRM 55-30-05.

Part: PLATE — CORRODED (STABILIZER) · airframe 33,888 hrs · 18,071 cycles

DURING HMV THE RT VERTICAL-TO-HORIZONTAL STABILIZER INBOARD AND OUTBOARD HINGE PLATES WERE FOUND WITH CORROSION IN THE BORES. A REPAIR WAS MADE AND APPROVED VIA FAA FORM 8100-9.

Part: SEAT TRACK — GOUGED (BS 588-759) · airframe 33,888 hrs · 18,071 cycles

CABIN SEAT TRACK GOUGED AND CORRODED OUT OF LIMITS FS 588-759 RBL 54. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01.

Part: SEAT TRACK — GOUGED (BS 439-519) · airframe 33,888 hrs · 18,071 cycles

CABIN SEAT TRACK GOUGED OUT OF LIMITS, FS 439-519 RBL 54. FABBED NEW SEAT TRACK AND INSTALLED, IAW MD90 SRM 53-40-01 VOL I.

Part: SEAT TRACK — GOUGED (BS 674-798) · airframe 33,888 hrs · 18,071 cycles

CABIN SEAT TRACK GOUGED AND CORRODED OUT OF LIMITS FS 674-798 RBL 22. REMOVED AND REPLACED DAMAGED SEAT TRACK, IAW MD90 SRM 53-40-01FIG 6 VOL I.

Part: CUSP WEB — CORRODED (BS 731-750) · airframe 33,888 hrs · 18,071 cycles

RT CUSP WEB 731-750 CORRODED AROUND FASTENERS. REPAIRED DAMAGED CUSP WEB, IAW MD90 SRM 51-30-08, ERA 398191-14MA DATE 09-18-02.

Part: SEAT TRACK — CORRODED (BS 486-551) · airframe 33,888 hrs · 18,071 cycles

CABIN SEAT TRACK GOUGED AND CORRODED OUT OF LIMITS FS 486-551 RBL.22, .058" REMAINING MATERIAL. REMOVED AND REPLACED SEAT TRACK FS 486-551 RBL 22, IAW MD90 SRM 51-30-01 AND SRM 53-40-01 FIG 6.

Part: CUSP WEB — CORRODED (STA 588 LBL 58) · airframe 33,888 hrs · 18,071 cycles

LT CUSP WEB HAS CORROSION STA 588 LBL 58. REPAIRED CUSP WEB IAW MD-80 SRM 53-05D FIG 827D ON N/R 2700-0226 AT HMV-2 IN OKC.

Part: SEAT TRACK — GOUGED (FS 585) · airframe 33,888 hrs · 18,071 cycles

CABIN SEAT TRACK GOUGED OUT OF LIMITS FS 585 LBL 22. REMOVED AND REPLACED DAMAGED PORTION OF SEAT TRACK IAW SRM 53-40-01 VOL 1 ON N/R 2700-0129 AT HMV-2 IN OKC.

Part: WEB — CRACKED (FS 210) · airframe 33,888 hrs · 18,071 cycles

L1 DOOR CUTOUT AFT SIDES FS 210 WEB FINGER CRACKED FWD FASTENER HOLE AT LONG 15. REPAIRED DAMAGE ON L1 DOOR CUTOUT AFT SIDE IAW MD-90 SRM 51-11-01 ON N/R 2000-0190 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (BS 939) · airframe 33,888 hrs · 18,071 cycles

RT CUSP WEB FS 939 CORRODED AT LIGHTNING HOLE. REPAIRED CUSP WEB IAW EA 53-05D ON N/R 2700-0149 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (BS 772) · airframe 33,888 hrs · 18,071 cycles

RT CUSP WEB CORROSION STA 772 RBL 58. REPAIRED CUSP WEB IAW ERA 413196-14MA DATE 5/15/03 ON N/R 2000-0140 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (BS 770) · airframe 33,888 hrs · 18,071 cycles

LEFT CUSP WEB FS 770 EXFOLIATED AT LIGHTENING HOLE. REPAIRED CUSP WEB, IAW DELATA REPAIR DOC NR 53-05D SHT 1 FIG 827D.

Part: CUSP WEB — CRACKED (BS 1357) · airframe 33,888 hrs · 18,071 cycles

FOUND RT CUSP CRACKED RBL 57 STA 1357. REPAIRED CUSP WEB IAW MD-90 SRM 51-11-01 VOL 2 ON N/R 2000-0136 AT HMV-2 IN OKC.

Part: DOOR FRAME — CORRODED (AFT CABIN) · airframe 33,888 hrs · 18,071 cycles

AFT MAIN ENTRY FOOL SHOWS EVIDENCE OF CORROSION. REPAIRED JAMB SECTION, IAW ERA 466167-14 REV ORIG 1-30-08.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 31,403 hrs · 16,659 cycles

THE RT UPPER SKIN PANEL ON THE HORIZONTAL STABILIZER WAS FOUND CRACKED. THE CRACKED SKIN WAS CUT OUT AND A NEW SKIN PANEL WILL BE INSTALLED WITHIN 2000 FLIGHT HOURS.

Part: CRANK ASSY — CRACKED (LEFT PYLON FLAP) · airframe 27,852 hrs · 14,665 cycles

LEFT PYLON FLAP ACTUATOR CONTROL ROD BRACKET IPC27-51-00-35 ITEM 145 CRACKED AT SPLINE BOSS CLAMPING AREA RESULTING IN LOSS OF MOVEMENT OF LEFT PYLON FLAP PANEL. MFG P/N 5966309-1. REPLACED SAME.

Part: OVEN — MALFUNCTIONED (FWD GALLEY) · airframe 26,641 hrs · 14,020 cycles

FORWARD GALLEY OVEN SMOKED WHEN TURNED ON. SMOKE DISSIPATED WHEN OVEN WAS SELECTED OFF. REPLACED OVEN.

Part: WIRE HARNESS — ARCED (CABIN) · airframe 25,219 hrs · 13,277 cycles

PAX NOTICED ARCING AND SMOKE FROM FLOOR NEAR 26C. INSPECTED AREA COULD NOT FIND DAMAGE BUT RT SIDE OF A/C AUDIO ENTERTAINMENT SYSTEM DEAD. REPLACED HARNESS AT ROWS 25-26 FOR ARCING DAMAGE.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE) · airframe 24,821 hrs · 13,077 cycles

PASSING 3000 FT RT ENGINE FIRE DETECTOR FAULT MESSAGE ILLUM IT STAYED ON FOR APPROX 1 MIN AND THEN WENT OUT. FIRE DET FAULT MESSAGE CAME ON WITH RT ENG B-LOOP LIGHT. LIGHT INTERMITTENT CAME ON AND OFF WITH WITH -B- LOOP. PERFORM FAULT TEST PER T/S MANUAL. NO FAULTS. SELECTED -A- LOOP AND PERFORM FIRE DETECTOR TEST. TEST GOOD. FWD THE RT ENGINE -B- LOOP TO MCO AND PLAC INOP PER MEL 26-11-01.

Part: PRESSURE SWITCH — INOPERATIVE (LT WW) · airframe 24,806 hrs · 13,068 cycles

WHILE TAXIING SLOWLY ARMED T/O MODE OF AUTOBRAKES A/C IMMEDIATELY AND ABRUPTLY STOPPED. RECEIVED AUTOBRAKE FAIL MESSAGE ON EOAP. NORMAL BRAKING OPERATES FINE. FAULTS IBCV1 SOV. REPLACED SAME.

Part: TIRE — CUT (NR 2) · airframe 24,317 hrs · 12,844 cycles

ITEM CUT IN NR 2 MAIN TIRE. REPLACED NR 2 MAIN WHEEL ASSY PER M/M.

Part: DIODE — INOPERATIVE (FLASHLIGHT) · airframe 23,899 hrs · 12,671 cycles

AFT EMERGENCY FLASHLIGHT LED INOP. REPLACED FLASHLIGHT AND BATTERY.

Part: COALESCER BAG — UNSERVICEABLE (RIGHT) · airframe 23,313 hrs · 12,391 cycles

AFTER T/O FLT ATTENDANT A/C LEFT MX HANGER. FUMES WERE NOT GETTING STRONGER BUT WERE MORE NOTICEABLE NEAR FLOOR. CONTINUED THROUGHOUT FLIGHT. ADVISED BY MAINT NOT TO START APU ON GROUND. REPLACED RT COALESCER BAG FOR T/S. PERFORMED PNEUMATIC HIGH PRESSURE BURNOUT PER MM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 22,868 hrs · 12,150 cycles

EMERGENCY CABIN LIGHT L2-746 WOULD NOT ILLUMINATE - FOUND A OPEN WIRE AT L2474A16N ALSO FOUND POWER SUPPLY B5-227 WITH A SUSPECTED BLOWN INTERNAL FUSE - REPAIRED WIRE AND REPLACED POWER SUPPLY / OPERATION NOW NORMAL.

Part: WIRE — CHAFED (CABIN) · airframe 20,570 hrs · 10,999 cycles

THE ORIGINAL WRITE UP HAPPENED IN ONTARIO. A/C NOW LOCATED MCI. DURING POWER TRANSFER FROM GROUND POWER TO SHIPS POWER SPARKS SEEN COMING FROM OVERHEAD BIN AT 12 C. AREA INSPECTED NO TROUBLE FOUND IN ONT. UPON ARRIVAL TO MCI PILOTS NOTICED C/B POPPED FOR PASSENGER OVERHEAD LIGHTS AND HANDRAIL LIGHTS ON RT SIDE OF A/C. TECHNICIANS PULLED DOWN OVERHEAD BIN BETWEEN 12C TO 15 C FOUND WIRES HAD CHAFED ON OVERHEAD BIN SUPPORT BRACKET AT 12C APPROX 1 FT FROM PLUG P5-3410 WIRES REPAIRED AND RELOCATED.

Part: DOOR SEAL — DIRTY (L2 DOOR) · airframe 20,200 hrs · 10,811 cycles

2L DOOR LEAK, CABIN ALTITUDE REACHED 10K FT. CHECKED 2L DOOR SEAL AND MATING SURFACE. NO DEFECTS NOTED. CLEANED 2L DOOR SEAL AND MATING SURFACE. PRESSURIZED ACFT TO 7 PSID. NO LEAKS/SQUEALS NOTED AT 2L.

Part: BRAKE — OVERHEATED (NR 2) · airframe 16,305 hrs · 8,811 cycles

AFTER LDG LT OUTBD BRAKE TEMP 575 LT INBD 500 DEGREES. LINEMAN REPORTED A FLAME FROM LEFT INBOARD BRAKE THAT WENT OUT AFTER A FEW SECONDS - REPLACED BRAKE

Part: ACTUATOR — LEAKING (RT MLG BUNGEE) · airframe 14,224 hrs · 7,682 cycles

HYDRAULIC LEAK IN RT MLG AREA. FOUND RT MLG BUNGEE ACTUATOR LEAKING WHILE RETRACTING GEAR. REPLACED SAME.

Part: ATTACH ANGLE — CRACKED (TAIL) · airframe 13,417 hrs · 7,247 cycles

RUDDER PCA ATTACH BRACKET STRUCTURE CRACKED. RUDDER PCA ATTACH BRACKET ALL BOLTS LOOSE. STOP DRILLED HOLE AND FABRICATE NEW BRACKET. SECURE BOLTS.

Part: PANEL — SEPARATED (NR 2 ENGINE)

ON ARRIVAL DFW FOUND NR 2 ENGINE C-DUCT ACCESS PANEL BLOWOUT DOOR MISSING. UPPER C-DUCT COWL DAMAGED BY DOOR. REPLACED UPPER REVERSER HALF AND RIGGED PER MM 78-32-00. REPLACED AND ADJUSTED BLOWOUT DOOR.

Part: GCU — FAILED (APU)

AT 31K FT APU GEN TRIPPED OFF LINE, RT ENG GEN ON MCO. A/C RETURNED. REPLACED APU GCU.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

LT ENG COMPRESSOR STALLED ON TAKEOFF. REPLACING LT ENGINE.

Part: SOCKET — BROKEN (CABIN)

PASSENGER SEAT 2C EMERGENCY TRACK LIGHTING DAMAGED. REPLACED SOCKET AND BULB, OPS NML. MCO AND PLAC REMOVED.

Part: TIRE — FAILED (RT MLG)

ON LANDING, NR 4 TIRE BLEW, RIGHT GEAR FLYING DOOR SEPARATED FROM AIRCRAFT. REPLACED NR 3 AND NR 4 WHEEL ASSYS AND FLYING DOOR.

Part: LIGHT WIRES — FAILED (AFT GALLEY)

BRIEF SPARKS, NO ACTUAL FIRE, ABOVE BALLAST IN CEILING AT AFT LEFT GALLEY. AREA WAS COOL TO TOUCH. FOUND SIXTEEN BURNED WIRES. REPAIRED ALL WIRES, ALL LIGHTS OPS CHECK.