N912DN

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,701 hrs · 32,550 cycles

LEFT OVER WING EMERGENCY EVACUATION LIGHT INOP. R&R LEFT AND RIGHT EXTERIOR EMERGENCY LIGHT ASSEMBLIES PER AMM 33-51. R&R POWER SUPPLY B5-125 PER AMM 33-51. ALL CHECK GOOD.

Part: ACCESS PANEL — DAMAGED (VERTICAL STAB) · airframe 59,296 hrs · 32,298 cycles

ELONGATE HOLES ON ACCESS PANEL 370TL ON THE VERTICAL STABILIZER. THE ACCESS PANEL WAS REPAIRED IAW ER/A 567293-14, REV ORIGINAL, AND ETI-90-18-022, REV 1.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 59,295 hrs · 32,297 cycles

CRACKED RT ANGLE TO ATTACH VERTICAL STABILIZER P/N 5912188-50 IN REF 5530-01034-0102. REPLACED PER SRM VOL I 51-30-02 AND 51-30-05.

Part: FLOOR PANEL — NOT REPORTED · airframe 59,295 hrs · 32,297 cycles

PERFORM PERMANET REPAIR PER ER/A 560348-14 REV ORIG FLOOR PANELS NBRS 221KF AND 221LF WERE FABRICATED, REPLACED AND IDENTIFIED PER VOL 1 SRM 53-20-03 PAR 5 AND ER/A 560348-14 REV ORIGINAL AND WERE INSTALLED PER ER/A 560348-14 REV ORIGINAL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,295 hrs · 32,297 cycles

AFTER REMOVE FLOOR PANELS IN REF LOG 3112788. CORROSION WAS FOUND ON AFT EVACUATION SLIDE LATCH SUPPORT X=-53 FROM STA Y=180 TO 200 AT FWD WET AREA. SLIDE LATCH SUPPORT WAS REPLACED PER SRM VOL II 51-30-01.

Part: POWER SUPPLY — DISCONNECTED (EMERGENCY LIGHTS) · airframe 58,005 hrs · 31,547 cycles

DURING A SERVICE CHECK, FOUND THE COCKPIT EMERGENCY LIGHT & AFT FACING EXIT SIGN OVER L1 JUMPSEAT INOPERATIVE. FOUND POWER SUPPLY B5-234 DISCONNECTED. CONNECTED AND OPS CHECKED GOOD. OK FOR SERVICE.

Part: RELEASE MECH — OUT OF ADJUST (TAILCONE) · airframe 57,482 hrs · 31,253 cycles

OUT OF CLEARANCE , CLAMPS FOR LOCKING CABLES DURING PULL TEST. ADJUSTED EMERGENCY RELEASE MECHANISM FOR TAILCONE.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,929 hrs · 30,396 cycles

AFT SIDE OF WEB, STA 1520 PULLEY CUT OUT CRACKED. REPAIRED IAW ERA 552963-14, REV O.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,929 hrs · 30,396 cycles

RIGHT HAND SIDE AFT LOUVER , STA 1520, L10R CRACKED. REPLACED ANGLE IAW DWG 9911839.

Part: SKIN — CRACKED (BS 1494) · airframe 54,402 hrs · 29,439 cycles

EMPENNAGE FUSELAGE SKIN IS CRACKED IN 3 AREAS BETWEEN, BS 1494, S2 LT-S4 LT. REPAIRED IAW ERA 546459-14, REV O.

Part: JACKSCREW — WORN (HORIZONTAL STAB) · airframe 54,402 hrs · 29,439 cycles

HORIZONTAL STABILIZER JACKSCREW THREADS WORN AT CENTER AREA. REMOVED AND INSTALLED JACKSCREW IAW AMDS 27-41-4591.

Part: DOOR FRAME — GOUGED (CARGO BIN) · airframe 50,706 hrs · 27,258 cycles

GOUGE ON FORWARD LOWER FRAME OF CARGO BIN DOOR. ACCOMPLISHED PRI 531222-14, REV 1.

Part: SUPPORT ANGLE — BROKEN (AFT STAIR) · airframe 49,006 hrs · 26,226 cycles

AFT VENTRAL STAIRS HAS A STEP SUPPORT ANGLE THAT IS BROKEN AND A NUT STRIP ANGLE THAT IS DAMAGED, LT SIDE OF STEP. CUT OUT DAMAGE SECTION. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 51-70-01, FIG 1 AND 51-30-02.

Part: LONGERON — CORRODED (BS 1344-1364) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO, UNDER WASTE WATER TANK, BS 1344-1364, LONGERON 27R, CORRODED. CUT OUT DAMAGE. FABRICATED AND INSTALLED SPLICE IAW SRM 51-30-05 AND 51-30-02.

Part: WEB — CORRODED (BS 1390) · airframe 49,006 hrs · 26,226 cycles

AFT CARGO BAY BS 1390, SUPPORT WEB HAS CORROSION ON FORWARD AND AFT FACE. CUTOUT DAMAGED WEBS. FABRICATED AND INSTALLED REPAIR SPLICES IAW ERA 523972-14, REV O.

Part: FRAME — CORRODED (BS 1379) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BILGE AREA, BS 1379 LONGERON 30, CORROSION ON FRAME, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLLED FORMER SECTION IAW SRM 53-10-02.

Part: LONGERON — CORRODED (BS 1324-1355) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BAY LONGERON 30 CORRODED BS 1324-1355. FOUND CORROSION TO BE OUT OF LIMITS. FABRICATED AND INSTALLED LONGERON AND SPLICE IAW SRM 53-10-01 AND DWG 5936667, REV CD.

Part: FRAME — CORRODED (BS 1231) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BAY FRAME CORRODED AT BS 1231, BETWEEN LONGERON 29 AND 30R. FOUND TO BE OUT OF LIMITS AFTER REWORK. FABRICATED AND INSTALLED FRAME AND SPLICE REPAIR IAW SRM 53-10-02, FIG 3, 51-10-03 AND 53-10-03.

Part: ANGLE — CRACKED (AFT) · airframe 49,006 hrs · 26,226 cycles

EMPENNAGE TOP RT ANGLE VERTICAL SKIN HAS CRACK BETWEEN 2 EA RIVETS JUST TOP SIDE OF RT AC GRILL. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SR09530296.

Part: FRAME — MISREPAIRED (BS 1344) · airframe 49,004 hrs · 26,225 cycles

REPAIR AT FRAME BS 1344, LONGERON 29L TO 29R NOT INSTALLED IAW SRM REFERENCE. REMOVED, FABRICATED AND INSTALLED NEW ANGLES IAW SRM 53-10-02, FIG 2.

Part: DOUBLER — CORRODED (AFT PRESS BLKHD) · airframe 49,004 hrs · 26,225 cycles

AFT PRESSURE BULKHEAD DOUBLER CORRODED, BS 1395, LONGERON 29R-29L, REMOVED DAMAGE. LOCATED, DRILLED AND INSTALLED NEW DOUBLER IAW SRM 51-30-05 AND DWG 9915561.

Part: DOOR FRAME — DAMAGED (CARGO BAY) · airframe 49,004 hrs · 26,225 cycles

MID CARGO BAY CUTOUT LOWER PLATE HAS NUMEROUS LOCATIONS OF CORROSION, GOUGES AND TOOL DAMAGE. REMOVED DAMAGED MID CARGO DOOR JAMB BEAM, LOCATED, DRILLED AND INSTALLED NEW IAW SRM 51-30-05, 51-30-02 AND DWG 5930481.

Part: FRAME — CORRODED (BS 164) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BILGE AREA, BS 164, LONGERONS 26-27R FRAME CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FRAME SECTION IAW SRM 53-20-02, 51-10-02.

Part: FLOOR SUPPORT — CORRODED (BS 160) · corrosion level 2 · airframe 49,004 hrs · 26,225 cycles

FLOOR SUPPORT CORRODED BS 160 BL 0. FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I, REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02, DWG 9936534, SRM 51-10-03, PAR 14 AND 21, VOL 2, AMM 51-00-01, AND INSTALLED IAW DWG 9936534.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 49,004 hrs · 26,225 cycles

FLOORBEAM BS 200 RBL 5-LBL 5 CORRODED. REMOVED CORROSION IAW SRM 51-30-02, VOL 2, AND FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I. REMOVED AND REPLACED FLOORBEAM IAW DWG 9936534, SRM 51-10-03 PAR 14 AND PAR 21, VOL 2, AMM 51-00-01, AND INSTALLED IAW SRM 51-30-02, VOL 2.

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 49,004 hrs · 26,225 cycles

CORROSION ON FLOOR SUPPORT MAIN CABIN, BS 180 XCW 35 LT. REMOVED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-30-02.

Part: FRAME — CORRODED (BS 1344) · airframe 49,004 hrs · 26,225 cycles

CORROSION ON FRAME BS 1344, LONGERON 29L-27R. BOTH SIDES OF FRAME, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FORMER SECTION IAW 53-10-02, FIG 2.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 49,004 hrs · 26,225 cycles

FLOORBEAM CORRODED BS 180, RBL 12-44, REMOVED CORROSION AND FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-02, SRM 51-30-05, VOL II, DWG 9936534, SRM 51-10-03, PAR 14 AND 21, VOL 2, AMM 51-00-01 AND INSTALLED IAW SRM 51-30-02, VOL II.

Part: FLOOR SUPPORT — CORRODED (BS 160) · corrosion level 2 · airframe 49,004 hrs · 26,225 cycles

FLOOR SUPPORT CORRODED BS 160 LBL 12. FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02, VOL 2, DWG 9936534, SRM 51-10-03, VOL 2, PAR 14 AND 21, AMM 51-00-01, AND INSTALLED IAW DWG 9936354.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 49,004 hrs · 26,225 cycles

FLOOR SUPPORT AT L-1 DOOR, BS 160-200, LBL 58 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02, VOL 2, DWG 9936534, SRM 51-10-03, AMM 51-10-00, AND INSTALLED IAW SRM 51-30-02, VOL 2.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 49,004 hrs · 26,225 cycles

FLOOR SUPPORT CORRODED AT SEVERAL AREAS BETWEEN BS 160-200, LBL 56. REMOVED CORROSION IAW SRM 51-10-03, VOL 2. FOUND TO BE OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I, REMOVED AND REPLACED IAW SRM 51-30-02, FIG 1, DWG 993634, SRM 51-10-03, VOL 2, AND INSTALLED IAW SRM 51-30-02, VOL 2.

Part: LONGERON FITTING — CORRODED (BS 1395) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BAY BS 1395, L29R END FITTING CORRODED. R & R LONGERON END FITTING IAW SRM 51-30-05, FIG 1.

Part: LONGERON FITTING — CORRODED (BS 1395) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BAY BS 1395, L29L END FITTING CORRODED. R & R IAW SRM 51-30-05, FIG 12.

Part: SHEAR PLATE — CORRODED (BS 1269-1276) · airframe 49,004 hrs · 26,225 cycles

BILGE AREA IN AFT CARGO BAY BS 1269-1276 BETWEEN L29-30R CORROSION ON SHEAR TIE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (BS 902-983) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR SEAT TRACK, LBL 56 FROM BS 902-983 HAS AREAS OF CORROSION, BARE METAL AND WORN. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: SHEAR TIE — CORRODED (BS 1307) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BAY BS 1307, BETWEEN L27-28R HAD CORROSION ON SHEAR TIE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE AND STRAP IAW SRM 53-10-02, FIG 3, 51-30-02 AND 51-10-03.

Part: SEAT TRACK — CORRODED (BS 200-579) · airframe 49,004 hrs · 26,225 cycles

CABIN SEAT TRACK HAD SEVERAL AREAS WITH CORROSION AT RBL 46 BETWEEN BS 200-579. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, 51-10-03 AND 51-10-00.

Part: FRAME — CORRODED (BS 1250) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BAY, CORROSION ON FRAME BS 1250, BETWEEN L29-30L. FOUND OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW FRAME IAW SRM 53-10-02, 51-30-01 AND 51-10-03.

Part: SHEAR TIE — CORRODED (BS 1328) · airframe 49,004 hrs · 26,225 cycles

AFT CARGO BAY BILGE AREA, BS 1328, BETWEEN L28 -29R SHEAR TIE CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SECTION OF SHEAR TIE IAW DWG 9919605 AND SRM 53-10-02, FIG 3 AND 51-30-02.

Part: STRUCTURE — CORRODED (CENTER FUEL CELL) · airframe 49,004 hrs · 26,225 cycles

UPPER FUSELAGE AT MAIN PASSENGER CABIN, RIGHT SIDE FUEL CENTER TANK CORRODED AT BS 954, RBL 55-46. REMOVED CORROSION, TREATED, PRIMED AND FILLED VOIDS IAW ERA 523958-14, REV O.

Part: STRUCTURE — CRACKED (BS 210) · airframe 49,004 hrs · 26,225 cycles

CRACK FOUND JUST AFT L1 DOOR, BS 210, L15L ON DOOR SURROUNDING STRUCTURE. CUTOUT DAMAGE. FABRICATED AND INSTALLED FILLER AND STRAP IAW SRM 51-30-02 ADN 53-60-02.

Part: SEAT TRACK — DAMAGED (BS 218-430) · airframe 49,004 hrs · 26,225 cycles

CABIN SEAT TRACK LBL 56, FROM BS 218 - 430, SEVERAL AREAS CORRODED, BARE METAL AND WORN. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED IAW SRM 53-40-01.

Part: FRAME — CORRODED (BS 168) · airframe 49,004 hrs · 26,225 cycles

FRAME BS 168 BETWEEN LONGERONS 17-19R, HAS CORROSION. REMOVED CORROSION. FABRICATED AND INSTALLED NEW FRAME STRAP IAW ERA 523963-14, REV O AND DWG 3921387.

Part: CUSP WEB — CORRODED (BS 840-864) · airframe 49,004 hrs · 26,225 cycles

CUSP WEB CORRODED AT LT AREA BETWEEN BS 840-864. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-20-02.

Part: SEAT TRACK — DAMAGED (BS 200-488) · airframe 49,004 hrs · 26,225 cycles

CABIN SEAT TRACK, LBL 46, BETWEEN BS 200-488, AREAS CORRODED, SCRATCHED AND BARE METAL. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK, SPLICE AND PLATE IAW SRM 53-40-01, FIG 6.

Part: SEAT TRACK — DAMAGED (BS 1155-1259) · airframe 49,004 hrs · 26,225 cycles

SEAT TRACK, LBL 46, FROM BS 1155 - 1259 CORRODED, WORN AND BARE METAL. FOUND CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-40-01, 51-30-01, AND 51-30-05.

Part: SEAT TRACK — DAMAGED (BS 1258-1363) · airframe 49,004 hrs · 26,225 cycles

CABIN SEAT TRACK, LBL 46, BS 1258 - 1363 CORRODED, SCRATCHED AND HAS BARE METAL IN SEVERAL AREAS. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, 51-30-01, AND 51-30-05.

Part: SEAT TRACK — DAMAGED (BS 1231-1363) · airframe 49,004 hrs · 26,225 cycles

SEAT TRACK, LBL 56 FROM BS 1231-1363 HAS AREAS WITH CORROSION, BARE METAL AND WORN. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-30-02, 53-40-01 AND 51-30-05.

Part: CUSP WEB — CORRODED (BS 618-640) · airframe 49,004 hrs · 26,225 cycles

LEFT CUSP WEB CORRODED BETWEEN BS 618-640. FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGE. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-20-02, FIG 13.

Part: CUSP WEB — CORRODED (BS 1245) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR CUSP WEB CORRODED AT TOP SIDE, BS 1245. FOUND OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02, FIG 13.

Part: CUSP WEB — CORRODED (BS 674-693) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR CUSP WEB LT CORRODED AT UPSIDE BETWEEN BS 674-693. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 734-754) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR CUSP WEB RT CORRODED AT UP SIDE BETWEEN BS 734-754. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 864-902) · airframe 49,004 hrs · 26,225 cycles

MAIN CABIN CUSP WEB CORRODED & CRACKED BETWEEN BS 864-902, CUTOUT DAMAGE. FABRICATED AND INSTALLED DOUBLER REPAIR IAW 53-10-03, FIG 9.

Part: CUSP WEB — CORRODED (BS 598-618) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR, LT CUSP WEB CORRODED AT BS 598-618. FOUND 100 PERCENT MATERIAL LOSS. CUTOUT DAMAGE. FABRICATED DOUBLER AND FILLER IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — CORRODED (BS 694-714) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR CUSP WEB RT CORRODED AT UPSIDE BETWEEN STA 694-714. FOUND CORROSION OUT OF LIMITS. CUTOUT DAMAGE. FABRICATED FILLER AND REPAIR SPLICES IAW SRM 53-20-02.

Part: SKIN — CORRODED (BS 1165) · airframe 49,004 hrs · 26,225 cycles

LEFT FUSELAGE SKIN UNDER RUBSTRIP AT BS 1165 HAS CORROSION. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-30-01.

Part: CUSP WEB — CORRODED (BS 540) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR CUSP WEB LBL 56 CORRODED AT BS 540. FOUND OUT OF LIMITS. FABRICATED DOUBLER AND FILLER REPAIR IAW SRM 53-20-02, FIG 10.

Part: CUSP WEB — DAMAGED (BS 845-864) · airframe 49,004 hrs · 26,225 cycles

CUSP WEB SCRATCHED TOP SIDE BETWEEN BS 845-864. BLENDOUT SCRATCHES. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 617-636) · airframe 49,004 hrs · 26,225 cycles

RT CUSP WEB CORRODED BETWEEN BS 617-636. REMOVED CUSP WEB. FABRICATED AND INSTALLED NEW CUSP WEB IAW DWG 9940443.

Part: CUSP WEB — CORRODED (BS 636-655) · airframe 49,004 hrs · 26,225 cycles

CUSP WEB RT, CORRODED BETWEEN BS 636-655. REMOVED CUSP WEB. FABRICATED AND INSTALLED NEW CUSP WEB IAW DWG 9940443, REV A.

Part: CUSP WEB — CORRODED (BS 655-674) · airframe 49,004 hrs · 26,225 cycles

CABIN FLOOR CUSP WEB CORRODED BETWEEN BS 655-674. REMOVED CUSP WEB. FABRICATED AND INSTALLED NEW CUSP WEB IAW DWG 9940443, REV A.

Part: FLOOR PANEL — CORRODED (BS 160-200) · airframe 49,004 hrs · 26,225 cycles

MAIN CABIN CENTER FLOOR PANEL CORRODED, BS 160-200 . CUTOUT DAMAGE, FABRICATED AND INSTALLED NEW FLOOR PANEL IAW ERA 523959-14, REV O AND SRM 51-11-01, FIG 2.

Part: SKIN — GOUGED (LT WING) · airframe 49,004 hrs · 26,225 cycles

LEFT WING EXISTING REPAIR DOUBLER HAS DEEP GOUGES BETWEEN NR 10 AND NR 11 SLAT TRACK. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED NEW EXTERNAL REPAIR IAW SRM 57-20-01, PARA 21 AND ERA 522710-14.

Part: STRUCTURE — CORRODED (CENTER FUEL CELL) · airframe 49,004 hrs · 26,225 cycles

UPPER FUSELAGE AT MAIN PASSENGER CABIN INTERNAL STRUCTURE BETRWEEN BS 902-984, LT SIDE FUEL CENTER TANK CORROSION. REMOVED CORROSION. FILLED VOID AND RESTORED VAPOR BARRIER IAW ERA 523957-14, REV O.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 49,004 hrs · 26,225 cycles

RT WING L/E HAS DAMAGED EXIT STRIP REPAIR BETWEEN STA XIS=50.5-XIS=68.5. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW ERA 523973-14, REV O.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,795 hrs · 24,903 cycles

OVERWING EXIT SIGN HAS NUMEROUS LAMPS OUT. REPLACED LAMPS. OPS CHECKED NORMAL.

Part: DOUBLER — DAMAGED (BS 598-617) · airframe 44,656 hrs · 23,694 cycles

DUE AT PSV CHECK, FOUND ACCESS DOOR STA 598-617 S-19R THRU S-21R. INTERNAL DOUBLER DAMAGE.

Part: FASTENER — LOOSE (FUSELAGE SKIN) · airframe 44,656 hrs · 23,694 cycles

INSPECTION OF SKIN PANEL FOUND SCREW LOOSE AND SEALANT TORN. REPLACED SCREW AND SEALED ARE PER SRM 51-30-2, COMPLIED WITH ERA 470202-14 REV O, COMPLIED WITH NR 1.

Part: COVER — LOOSE (R1 DOOR SLIDE) · airframe 44,258 hrs · 23,475 cycles

FLIGHT CREW FOUND R1 DOOR SLIDE COVERING LOOSE. MAINTENANCE CONNECTED SLIDE LANYARD. OPERATION CHECKS GOOD.

Part: DOOR — BENT (L1) · airframe 43,677 hrs · 23,153 cycles

OPERATIONS REPORTED L1 DOOR LOWER EDGE BENT. MAINTENANCE STRAIGHTENED L1 DOOR LOWER EDGE PER SRM 52-01-01. AIRCRAFT IS OKAY FOR SERVICE.

Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 43,542 hrs · 23,095 cycles

FLIGHT CREW REPORTED DOOR 1R SLIDE LANYARD DETACHED. MAINTENANCE INSTALLED LANYARD. AIRCRAFT OKAY FOR SERVICE.

Part: FASTENER — LOOSE (VERTICAL STAB) · airframe 41,360 hrs · 22,044 cycles

SCREWS ARE LOOSE ON L/E OF VERTICAL STAB. REPAIRED PER EA 02-470871-12 REV A ME-05.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,357 hrs · 22,042 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT DAMAGED. MISSING LIGHT, HOUSING BROKEN AND WIRE SPLICE SEPARATED. MAINTENANCE SPLICED THE WIRES AND REPLACED THE BULB HOUSING AND THE BULB PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,332 hrs · 22,034 cycles

CABIN ATTENDANT FOUND TWO FLOOR EMERGENCY PATHWAY LIGHTS BROKEN BY ROW 5. MAINTENANCE REPLACED LIGHT ASSEMBLIES AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THEM.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 37,599 hrs · 20,131 cycles

THE HORIZONTAL STABILIZER RT UPPER AFT SKIN PANEL DAMAGED. REPAIRED IAW ERA 477402-14.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 37,599 hrs · 20,131 cycles

CRACKS FOUND IN THE HORIZONTAL STABILIZER RT UPPER AFT SKIN PANEL. REPAIRED IAW 02-460214-12, ME06 02-460214-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,767 hrs · 21,341 cycles

DURING CHECK VIDEO CONTROL UNIT EMERGENCY LIGHTING FLOOR LIGHTS INOPERATIVE. ITEM WAS FWD TO MCO/PLACARD ON 16AUG10. THEN ON 18AUG10 MSP MX REPAIRED BROKEN WIRE AT 10CDE. ALL FLOOR PATH LIGHTS NOW OPERATE NORMAL AND THE MCO/PLACARD WAS REMOVED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 38,516 hrs · 20,651 cycles

CABIN FLOOR EMERGENCY ESCAPE PATH LIGHTS INOP FROM SEAT 10 TO 12. FOUND BROKEN WIRE AT SEAT 10. REPAIRED WIRE REF SWPM CH 20, LIGHTS CK OK.

Part: MONITOR — OVERHEATED (SEAT 25AB) · airframe 36,699 hrs · 19,663 cycles

VIDEO UNIT OVER 25A AND 25B OVERHEATED AND STARTED SMOKING. FLT ATTENDANTS REMOVED POWER FROM UNIT AND SMOKE AND BURNING SMELL WENT AWAY. UNIT COOLED DOWN. INSPECTION FOUND SOURCE OF SMOKE TO BE AT OVHD MONITOR AT 25 A/B. REMOVED AND CAPPED CONNECTOR TO MONITOR AT 25 A/B. TRANSFERRED VIDEO SYSTEM TO NEF 233-143CN PER CREW REQUEST FOR FURTHER TROUBLESHOOTING C/B ON ROW F LOCATION 2 BEHIND CAPT PULLED AND COLLARED.

Part: FITTING — CRACKED (LEFT WING) · airframe 33,965 hrs · 18,040 cycles

LEFT WING GROUND SPOILER PANEL O/B HINGE MOUNT FITTNG IS CRACKED. REMOVED AND REPLACED FITTING, IAW MD90 SRM 51-30-02.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 33,965 hrs · 18,040 cycles

FWD CARGO PIT LWR DOOR JAMB IS CORRODED AROUND MULTIPLE FASTENER HOLES. REPAIRED DOOR JAMB, IAW MD80 SRM 53-05D.

Part: SKIN — DENTED (CARGO DOOR) · airframe 33,965 hrs · 18,040 cycles

AFT CARGO DOOR FRONT SKIN HAS SEVERAL DENTS. REPAIRED DENT IN CARGO DOOR, IAW MD80 SRM 52-05D, FIG 3. ALL OTHER DENTS COND 1A, IAW MD90 SRM 53-30-02, PG 11 TABLE 3.

Part: SKIN — CORRODED (BS 792-876 L29R) · airframe 33,965 hrs · 18,040 cycles

FOUND FUSELAGE SKIN CORRODED 792 TO 876 LONG 29R. REPAIRED FUSELAGE SKIN, IAW MD80 SRM 53-04 FIG 53.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

AFT VENTRAL DOOR JAMB HAS CORROSION ON LOWER SECTION AT SEAL ATTACHMENT AREA. REPAIRED AFT VENTRAL DOOR JAMB, IAW DELTA ER/A 467131-14 REV ORIG. 03-25-08 VIA EA 12541, REV I/R 03-25-08.

Part: SHEAR TIE — CORRODED (CARGO BAY) · airframe 33,965 hrs · 18,040 cycles

FOUND CORROSION ON FRAME Y 1193.0 AT 30L. REMOVED AND REPLACED SHEAR TIE, IAW MD90 SRM 51-30-02 AND 51-30-05.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 33,965 hrs · 18,040 cycles

RIGHT WING I/B FLAP HAS A SHARP DING ON LOWER SURFACE JUST AFT OF NUMBER 3 TIRE. FABRICATED AND INSTALLED NEW SKIN, IAW MD90 SRM 57-03D FIG 807D.

Part: SKIN — DENTED (TE FLAP) · airframe 33,965 hrs · 18,040 cycles

C/W ER/A 096112-14 REPAIR LEFT WING INBOARD MAIN FLAP LOWER SKIN X1F1=41.5 DENT. REPAIRED LEFT WING INBOARD MAIN FLAP LOWER SKIN, IAW ER/A 096112-14 REV B 01-28-06 AND MD90 SRM 57-03D FIG 807D PERMANENT REPAIR. NO FURTHER ACTION REQUIRED.

Part: CUSP WEB — CORRODED (BS 984-4003) · airframe 33,965 hrs · 18,040 cycles

LT CABIN CUSP WEB FS 984-1003 CORRODED. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01 FIG 2.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK RBL 54.5 OUT OF LIMITS, FS 731. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 760-899. REMOVED AND REPLACED SEAT TRACK FS 760-899, IAW MD90 SRM 53-40-01 FIG 6.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRK RBL 54.5 OUT OF LIMITS FS 1144-1316. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 972-1090. REMOVED AND REPLACED SEAT TRACK FS 899 TO 1090, IAW MD90 SRM 53-40-01 FIG 6.

Part: FITTING — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

REMOVED AND REPLACED FITTING, IAW MD90 SRM 51-30-01, 51-30-02 AND 51-10-05.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

FOUND CABIN SEAT TRACK RBL 54.5 OUT OF LIMITS, 1022-1050. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

FOUND CABIN SEAT TRACK RBL 54.5 OUT OF LIMITS, 590-674.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK RBL 22 OUT OF LIMITS, 1210-1364. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I.

Part: CUSP WEB — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CUSP WEB AT FS 830 LBL 54.5 HAS PREVIOUS DAMAGE CONSISTING OF 2 EA DRILL STARTS. REMOVED AND REPLACED WEB, IAW MD90 SRM 51-30-01 AND 51-30-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LT CABIN CUSP WEB FS 568-572 CORRODED. CUTOUT DAMAGED AREA, FABRICATED REPLACEMENT WEB DOUBLER AND INSTALLED, IAW MD90 SRM 53-05D, FIG 827D.

Part: CUSP WEB — BENT (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LEFT FUSELAGE CUSP "T" CHORD WAS FOUND BENT BETWEEN FS 902 AND 924_LBL 60. REMOVED, FABRICATED AND INSTALLED "T" CHORD, IAW MD90 SRM 51-30-02.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK LBL 54.5 HAS AREAS WITH NICKS, GOUGES, CORROSION AND BARE METAL FROM FS 196.25 TO FS 1364. REMOVED DAMAGE, FOUND THE FOLLOWING OUT OF SRM LIMITS: FS 421-620, 761-890 AND 1051-1090. ALL OTHER AREAS WITHIN SRM LIMITS, 53-40-01 FIG 4. ALL REPAIRS TO BE ACCOMPLISHED ON 1003548-2000.0228, 2000.0229, 2400.0230 AND 2400.0231.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LT CABIN CUSP WEB FS 659 CORRODED AT LIGHTENING. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01 FIG 2 VOL I.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK RBL 54.4 OUT OF LIMITS FS 503-550. REMOVED AND REPLACED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK RBL 22 OUT OF LIMITS, 588-864. REMOVED AND REPLACED DAMAGED SEAT TRACK RBL22 588-864, IAW MD90 SRM 53-40-01.

Part: SEAT TRACK — GOUGED (BS 1145-1153) · airframe 33,965 hrs · 18,040 cycles

FOUND CABIN SEAT TRACK RBL 22 OUT OF LIMITS FS 1145-1153. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 FIG 6 VOL 1.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK LBL 22 OUT OF LIMITS 3 AREAS FS 731 TO 769. REPAIRED CABIN SEAT TRACK, IAW MD90 SRM 53-40-01 FIG 6.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LONGERON 29.5R CORRODED FROM Y-1268.0 TO Y-1276.5. REMOVED CORROSION NO NOTABLE LOSS. TREATED AND PRIMED, IAW MD90 SRM 51-10-03. INSTALLED FASTENERS, IAW MD90 SRM 51-30-05 VOL II.

Part: VANE — DENTED (LT WING TE FLAP) · airframe 33,965 hrs · 18,040 cycles

LT WING I/B FLAP FIXED VANE LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED LT WING I/B FLAP I/B VANE, IAW MD90 SRM 57-50-04.

Part: FRAME — GOUGED (BS 1364) · airframe 33,965 hrs · 18,040 cycles

BS 1364 FROM LONG. 28R TO 24L THERE IS EDGE DAMAGE FROM FLOORBOARD FASTENERS (AFT CARGO BAY UNDERNEATH AFT BULKHEAD). BLENDED GOUGES, CHECKED LIMITS. OUT OF LIMITS IN SEVERAL PLACES. REMOVED SECT. OF FRAME, SPLICED NEW SECT. IN IAW MD90 SRM 51-10-10, 53-00-01, 51-3-02 AND 53-10-02D.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LT CUSP WEB CABIN FS 683-690 CORRODED. BLENDED CORRODED AREA, FOUND TO BE OUT OF LIMITS AND REPAIRED, IAW MD90 SRM 53-10-02, 51-10-03 AND MD80 DRD 53-05D FIG 827D.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LEFT CABIN CUSP WEB FS 1241, CRACKED AT GALLEY LINE SUPPORT ATTACHMENT. REPAIRED CRACKED CUSP WEB, IAW MD80 DRD 53-05D, FIG 827D.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LT CABIN CUSP WEB FS 584 CORRODED AT LIGHTENING HOLE ON UNDERSIDE. REPLACED LT CABIN CUSP WEB FS 584, IAW MD90 SRM 51-10-05.

Part: LONGERON — CORRODED (29R) · airframe 33,965 hrs · 18,040 cycles

FOUND LONGERON R29 CORRODED AT Y-1344.0. BLENDED CORROSION ON LONG R29, OUT OF LIMITS. REMOVED DAMAGED SECTION, INSTALLED NEW SECTION AND SPLICES IAW MD90 SRM 53-00-01, 51-30-02, 51-30-03 AND 53-10-01 (STA 1338 TO 1374).

Part: SEAT TRACK — GOUGED (BS 410-588) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 410-588, LBL 54.5 IAW MD90 53-40-01, FIG 6. REMOVED AND REPLACED SEAT TRACK STA 410 TO 588, LBL 54.5 IAW MD90 53-40-01, FIG 6.

Part: SKIN — DENTED (BS 218 S18L) · airframe 33,965 hrs · 18,040 cycles

C/W SRM 53-30-01 REPAIR FUSELAGE SKIN DENT STA 218 BELOW STR L-18. REPAIR FUSELAGE SKIN STA 218 BELOW STR L-18, IAW MD80 SRM 53-04D FIG 12B.

Part: SKIN — GOUGED (RT WING) · airframe 33,965 hrs · 18,040 cycles

REPAIR ON RT WING L/E STA XCW 121 IS GOUGED. REPAIRED RT WING L/E, IAW DELTA ERA 467132-14 REV ORIG DATE ISSUED 26MAR08 VIA AAR EA 12567 REV I/R DATE ISSUED 26MAR08.

Part: SEAT TRACK — GOUGED (BS 588-627) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 588-627. REMOVED AND REPLACED SEAT TRACK STA 588-627 LBL 54.5, IAW MD90 SRM 53-40-01, FIG 6.

Part: VANE — DENTED (LT WING TE FLAP) · airframe 33,965 hrs · 18,040 cycles

LT WING I/B FLAP O/B FIXED VANE LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED LT WING INBD FLAP O/B FIXED VANE, IAW MD90 SRM 51-50-04.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LT CABIN CUSP WEB FS 910-918 CORRODED. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER IAW DRD 53-05D, FIG 827D.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

RT GEAR WHEEL WELL CUTOUT FWD FRAME EXISTING REPAIR AT I/B END CRACKED. REMOVED AND REPLACED 5930584412 CHANNEL, IAW MD90 SRM 51-10-05.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,965 hrs · 18,040 cycles

CABIN SEAT TRACK FS 1321 LBL 44.5 CORRODED OUT OF LIMITS (100 PERCENT MATERIAL LOSS). REMOVED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK, IAW MD90 SRM 53-40-01 FIG 6.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 33,965 hrs · 18,040 cycles

LT CABIN CUSP WEB FS 1358 CRACKED AT LIGHTNING HOLE. REPAIRED LT CABIN CUSP WEB AT STA 1358, IAW MD9 SRM 51-11-01, TAGGED, IAW DELTA PROCESS STANDARD 900-5-1 NR 4.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,965 hrs · 18,040 cycles

UPON REMOVAL OF CABIN FLOORS FOR SEAT TRACK REPAIRS, ADDITIONAL CORROSION DAMAGE WAS FOUND OUT OF LIMITS ON THE FLOOR MATING FLANGE OF SEAT TRACK LBL 22 FS 1250 TO 1344. REMOVED AND REPLACED SEAT TRACK, IAW MD90 SRM 51-30-01.

Part: SKIN — DENTED (CARGO DOOR) · airframe 33,965 hrs · 18,040 cycles

MID CARGO DOOR, FOUND TO BE AFT SECTION, SKIN DENTED 12 INCHES FROM RIGHT AND 14.5 INCHES FROM TOP. REPAIRED, IAW MD90 SRM 51-00-01 AND MD80 SRM 52-05D.

Part: SKIN — DENTED (BS 195 L21R) · airframe 33,965 hrs · 18,040 cycles

C/W ERA 454243-14 REPAIR FUSELAGE SKIN FS 195 L-21R. REPAIR OF DENT AND GOUGE. REMOVED DAMAGED AREA, IAW MD90 SRM 53-30-01. INSTALLED REPAIR DOUBLERS AND FILLER, IAW MD90 SRM 53-30-01 FIG 1.

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 30,397 hrs · 16,039 cycles

ON DEPARTURE FROM BNA, AIRCRAFT SUFFERED COMPLETE ELECTRICAL POWER LOSS. FLIGHT CREW WAS ABLE TO START THE APU AND RECOVER THE RIGHT BUSS BUT NEVER THE LEFT. LT GEN DISCREPS FWD TO ITEM 5 THIS LOG. FOUND NUMEROUS FAULT LOGGED FOR RT GEN. GEN APPEARS NOT TO BE TURNING AND WOULD TAKE BUSS. REPLACED RT VSCF GEN PER MM. LEAK AND OPS CK GOOD. REPLACED EPCU AS PRECAUTION. ALL BUSSES CK OK. PERFORMED EPCU PER M/ FLUSHED COOLER PER M/M . FOUND OAP MSG LT GEN DIODE FAIL. REPLACED LT GEN PER M/M. OP AND LEAK CK GOOD. RESERVICED GEN.

Part: BALLAST — BURNED (CABIN) · airframe 29,194 hrs · 15,354 cycles

SMOKE COMING OUT OF PSU UNIT 26 CDE FOR 2 MINUTES, SMOKE THEN DISSIPATED. FOUND ONE SIDEWALL FLUORESCENT LAMP INOP AT ROW 26R. REMOVED PANEL AND INSPECTED SAME. RISIDUAL SMELL PRESENT WITH NO OTHER PROBLEMS FOUND. SUSPECT LIGHT BALLAST. FWD TO MCO AND PLAC. REINSTALLED PANEL. REPLACED BURNT BALLAST, LIGHT CKS GOOD. MCO/PLAC REMOVED.

Part: SKIN — CRACKED (BS 1475, L-1R) · airframe 28,252 hrs · 14,786 cycles

FUSELAGE CROWN SKIN PANELS ARE CRACKED AT THREE LOCATIONS NEAR STA 1475, L-1R. REMOVED DAMAGED SKIN AND INSTALLED A DOUBLER.

Part: STARTER — FAILED (APU) · airframe 25,830 hrs · 13,526 cycles

AFTER APU START ELECTRICAL SMELL IN CABIN. APU STARTER FAILED. REPLACED APU STARTER.

Part: GENERATOR — FAILED (RIGHT) · airframe 22,982 hrs · 12,128 cycles

RT AC FEEDER FAULT RT ELEC SYSTEM FAIL AND RT GEN OFF MESSAGE ON EOAP. WOULD NOT RESET IN FLT. FOUND METAL IN GENERATOR OIL. REPLACED GENERATOR.

Part: APU — FAILED (APU BAY) · airframe 22,948 hrs · 12,107 cycles

APU ELECTRONICS FAILED 45 MIN AFTER T/O. REPLACED APU AND DOOR ASSY.

Part: SENSOR — INTERMITTENT (NR 1 SLAT TRACK) · airframe 21,070 hrs · 11,162 cycles

AFTER T/O SLAT DISAGREE LIGHT REMAINED ON AFTER SLATS WERE RETRACTED. FOLLOWED POM PROCEDURE. FOUND LT WING SLAT SENSOR C D1-64 TO BE INTERMITTENT. REMOVED AND REPLACED SAME PER M/M. CYCLED FLAPS SEVERAL TIMES. ALL INDICATIONS NORMAL.

Part: TRANSFORMER — FAILED (E/E BAY) · airframe 20,500 hrs · 10,889 cycles

WHILE RELOCATING THE A/C FROM THE PAD TO THE GATE, OPS REPORTED SMOKE/ODOR IN CABIN. DL MTC FOUND THE NR 1 T/R HAD FAILED AND SMOKED. INSULATION ABOVE THE T/R WAS BURNED. REPLACED T/R UNIT.

Part: SEAL — LOOSE (COCKPIT WINDOW) · airframe 18,681 hrs · 9,973 cycles

LOUD VIBRATION PASSING THRU 10,000 FT ON CAPTAINS WINDOW SIDE. FOUND AERODYNAMIC SEAL LOOSE ON CAPTAINS WINDOW ON THE UPPERSIDE. REMOVED LOOSE SEAL. APPLIED NEW SEALER PER M/M.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 18,479 hrs · 9,872 cycles

FRAME CLIP FOUND CRACKED DURING HMV-1 AND WAS BEING REPLACED. BHEC INSPECT REVEALED A CRACK INDICATION.

Part: LIGHT — MISSING (CABIN) · airframe 18,391 hrs · 9,829 cycles

ONE CLEAR EMERGENCY FLOOR TRACK LIGHT WAS MISSING. REPLACED COVER, OPS NORMAL.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 16,242 hrs · 8,744 cycles

WHEN THROTTLES WERE RETARDED AT APPROX 16K RT PNEU SYS FAULT LIGHT ILLUMINATED ON OAP. POM PROCEDURES COMPLIED WITH NO EFFECT. ACCOMPANIED BY F/A REPORT OF A BURNING ELECTRICAL SMELL IN AFT CABIN AREA. REPLACED RECIRC FAN.

Part: ACCESS DOOR — NOT CLOSED (FUSELAGE) · airframe 13,354 hrs · 7,229 cycles

DURING CLIMBOUT, FLT ATTENDANT REPORTED A LOUD VIBRATION ON RIGHT SIDE OF THE AIRCRAFT. SUSPECT THE LEFT VSCF ACCESS DOOR CAME OPEN. RETURNED TO DFW. CLOSED VSCF CONVERTER DOOR. INSTALLED TIME LIMITED REPAIR PER ERA 377958-14.

Part: ANGLE — CRACKED (BS 1520)

THE LT VERTICAL STABILIZER-TO-FUSELAGE ATTACH ANGLE WAS FOUND WITH A 1.5 INCH LONG CRACK AT FS 1520. THE CRACK IS TYPICAL OF THAT FOUND IN MD-88 SRM 53-05, FIG 23. THE CRACKED HORIZONTAL FLANGE WAS CUTOUT AND REPAIRED WITH A STEEL ANGLE FABRICATED FROM A NEW PART. THE REPAIR WAS ACCOMPLISHED PER ER/A 367626-14.

Part: BULB — MISSING (CABIN)

EMERGENCY TRACK LIGHT 2C INOP. REPLACED SOCKET BULB AND LENS, OPS CHKS GOOD. REMOVED MCO AND PLAC.