N907DA

Part: LANDING GEAR — MALFUNCTIONED · airframe 62,522 hrs · 34,303 cycles

SHIP 9207 - GEAR - ON APPROACH UNABLE TO MOVE THE LANDING GEAR HANDLE DOWN. GEAR EXTENDED USING ALTERNATE EXTEND AFTER WHICH LANDING GEAR HANDLE WAS ABLE TO BE MOVED DOWN - ALTERNATE HANDLE STOWED AND GEAR DOORS RETRACTED - UNEVENTFUL LANDING WITH THREE GREEN. CORRECTIVE ACTION: SWUNG GEAR AND PERFORMED MECHANICAL GEAR CHECKS. NTF. REPLACED LANDING GEAR CONTROL VALVE AS PRECAUTION. PERFORMED SUCCESSFUL VERIFICATION FLIGHT. (LP# 5063416)

Part: CABLE — DISCONNECTED (L1 DOOR) · airframe 62,241 hrs · 34,108 cycles

DOOR 1L GIRT BAR CABLE IS DISCONNECTED. REINSTALLED CABLE INTO GIRT BAR, REF AMM 25-61. OK FOR CONT SERVICE.

Part: DOOR — DAMAGED (RAM AIR) · airframe 61,705 hrs · 33,739 cycles

A CRACK WAS FOUND ON THE FWD UPPER CORNER OF RAM ACCESS DOOR LAND STRUCTURE. REPAIRED IAW SRM 55-30-03, VOL 1.

Part: ACM — SEIZED (LEFT) · airframe 61,400 hrs · 33,566 cycles

AT THE GATE, USING HUFFER AIR, HOT AIR ODOR AND REPORTED HAZE IN THE CABIN. AFTER STARTING THE NR 1 ENGINE, DISCONNECTED EXTERNAL AIR AND SWITCHED TO ENGINE AIR, CABIN AIR SUPPLY TEMP HIGH. ENGINE SHUTDOWN. LEFT ACM FOUND LOW ON OIL, RIGHT ACM FOUND TO BE LOCKED UP. REPLACED BOTH ACMS AND COMPLIED WITH ODI PREVENTION PROCEDURES. COMPLETED VF WITH NO ISSUES.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 61,383 hrs · 33,557 cycles

ON LANDING, THE FLIGHT CREW STARTED THE APU WHILE TAXING TO THE GATE. SMOKE ODOR STARTED TO FILL THE PASSENGER CABIN. CREW SHUTDOWN THE APU AND THE SMOKE ODOR DISSIPATED. FOUND A HYDRAULIC LINE AT THE ANTI-SKID RETURN SOV LEAKING IN LEFT WHEEL WELL. SECURED THE LINE. PERFORMED MINI DUCT BURNOUT AND REPLACED COALESCER BAGS.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 61,298 hrs · 33,510 cycles

RT HORIZONTAL STAB UPPER REAR SPAR AFT BARREL NUT HOLE HAD A CRACK INDICATION, .250 INCHES LONG, RUNNING AFT AND DOWN INTO BARREL NUT HOLE. HFEC VERIFIED CRACK IAW NDTSPM 06-10-01.001. HORIZONTAL STABILIZER REPLACED IAW AMDS 5510-4001.

Part: CONTROL HANDLE — JAMMED (COCKPIT) · airframe 60,658 hrs · 33,145 cycles

GEAR HANDLE JAMMED IN UP POSITION. EMERGENCY GEAR EXTENSION PERFORMED LANDING WITH GEAR DOORS OPEN. OPENED TURTLE SHELL FOR ACCESS TO GEAR HANDLE (542278). FOUND GEAR HANDLE IN DOWN POSITION. PERFORMED DETAILED INSPECTION OF GEAR HANDLE MECHANISM, NO FAULTS NOTED. CHECKED ALL RIG PIN HOLES FOR ALIGNMENT, NO FAULTS NOTED. SWUNG GEAR NUMEROUS TIMES WITH NO ISSUES. MC & TA ADVISED. REMOVED AND STARTED TO INSTALL LANDING GEAR CONTROL VALVE PER MD90 AMM 32-31-01. COMPLETED INSTALLATION OF L/G CONTROL VALVE OPS AND LEAK CHECK OK. INSPECTED CABLES AND SLANTED PANEL, ALL FAIRLEADS CK. NO SIGNS OF WATER OR ICE. (486835). REPLACED BOTH GEAR DOOR SKID PLATES.

Part: COVER — BROKEN (EXIT SIGN) · airframe 59,437 hrs · 32,412 cycles

EMERGENCY EXIT SIGN COVER DOOR 1R BROKEN. SIGN REPLACED.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 58,786 hrs · 32,045 cycles

LEFT STRUCTURE AROUND JACKSCREW CRACKED. REPAIRED IAW ERA 559425-14.

Part: FRAME SPLICE — NOT REPORTED (NOT REPORTED) · airframe 58,786 hrs · 32,045 cycles

FRAME SPLICE LONGERONS 26 - 27L. COMPLIED WITH PRI/ERA 55943-14.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 58,786 hrs · 32,045 cycles

RIGHT STRUCTURE AROUND JACKSCREW CRACKED. COMPLIED WITH ERA 559425-14.

Part: FRAME — CORRODED (BS 1364) · airframe 58,786 hrs · 32,045 cycles

CORROSION ON FRAME AND SPLICES AT BS 1364 BETWEEN 29L AND 29R. REPAIRED IAW DWG SR9530057.

Part: MOTOR — WORN (RUDDER) · airframe 58,778 hrs · 32,040 cycles

UPPER AND LOWER PULLEY FOR RUDDER BELOW YAW DAMPENER MOTOR WORN.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,037 hrs · 31,634 cycles

EMERGENCY LIGHT FROM ROW 32 BACK REMAIN ON IN ARM POSITION. FOUND BAD POWER SUPPLY FOR LIGHTS. REPLACED BATTERY AND POWER SUPPLY B5-237 PER MM.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 57,865 hrs · 31,551 cycles

EMERGENCY LIGHTS IN AFT CABIN FLASHING WHEN ARMED. RESET THE EMERGENCY LIGHTS IAW MM.

Part: LIGHT — UNSECURE (CABIN) · airframe 57,741 hrs · 31,483 cycles

EMERGENCY LIGHT DAMAGED. SECURED THE LIGHT. OPERATION CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,671 hrs · 31,440 cycles

EMERGENCY LIGHTS OUT AT ROWS 34 AND 35. REMOVED AND REPLACED BATTERY PACK IAW AMM. OPS CHECK GOOD. (LP# 9039441)

Part: CONNECTOR — LOOSE (CABIN) · airframe 57,372 hrs · 31,259 cycles

L1 DOOR LOWER EMERGENCY EXIT IDENTIFIER INOPERATIVE. FOUND LOOSE CONNECTOR. RESECURED. OPERATION CHECKS GOOD.

Part: STRAP — FRAYED (TAILCONE SLIDE) · airframe 57,198 hrs · 31,164 cycles

TAILCONE SLIDE FORWARD HOLD DOWN STRAP FRAYED. REMOVED AND REPLACED THE STRAP IAW AMDS 5352-7116.

Part: UNKNOWN — SMOKE (CABIN) · airframe 55,607 hrs · 30,232 cycles

THE FLIGHT CREW REPORTED SMOKE IN THE CABIN DURING ENGINE START. PASSENGERS DEPLANED. SUSPECT SOURCE OF SMOKE TO BE THE AIR START CART. MAINTENANCE OPERATED BOTH AIR CONDITIONING PACKS AND STARTED BOTH ENGINES WITH NO SMOKE GENERATED. MAINTENANCE PERFORMED A BURNOUT OF THE PNEUMATIC HIGH PRESSURE DUCTING IAW AMM AND REPLACED BOTH COALESCER BAGS AS A PRECAUTION. ALL SYSTEMS NORMAL AND ACFT WAS RETURNED TO SERVICE.

Part: LANYARD — DAMAGED (L1 DOOR SLIDE) · airframe 54,576 hrs · 29,571 cycles

FOUND L1 DOOR SLIDE LANYARD UNSERVICABLE. REPLACED LANYARD.

Part: CUSP WEB — CRACKED (BS 962) · airframe 53,825 hrs · 29,105 cycles

CUSP WEB AT BS 962, RT FOUND CRACKED, REPAIRED IAW SRM 53-20-02, VOL I.

Part: FRAME — GOUGED (RT MLG DOOR) · airframe 53,825 hrs · 29,105 cycles

RIGHT MLG DOOR, FWD FRAME, FWD OTBD EDGE, GOUGED. REPLACED DOUBLER IAW DWG 5930584.

Part: FRAME — CRACKED (BS 962) · airframe 53,825 hrs · 29,105 cycles

CRACK IN RADIUS OF FRAME TAB OF RT OVERWING FRAME BS 962. REPLACED FRAME REF; AMDS 5310-01375-09-RT AND REWORK DWG SR-90530027 AND DWG CONFIG -7001.

Part: SKIN — CRACKED (FUSLEAGE) · airframe 53,825 hrs · 29,105 cycles

FUSELAGE SKIN CRACKED AT NOSE W/W RT AFT DOOR AFT HINGE CUTOUT. REPAIRED REF SRM 53-30-01, FIG 17 VOL 1.

Part: SKIN — CRACKED (BS 1474) · airframe 53,825 hrs · 29,105 cycles

BS 1474, STR 2L SKIN CRACKED UNDER SHEAR CLIP. REPAIRED IAW ERA 538124-14, REV ORIG.

Part: FITTING — CRACKED (BS 1494) · airframe 53,825 hrs · 29,105 cycles

TAIL INTERIOR UPPER BATH TUB FITTING CRACKED AT BS 1494, AFT SIDE OF FRAME LBL 6. R & R IAW DWG5930609.

Part: PRESSURE SWITCH — FAILED (CABIN PRESSURE) · airframe 52,346 hrs · 28,185 cycles

AFTER TAKE OFF, BOTH AIR CONDITIONING PACKS SHUTDOWN AND ACFT STOPPED PRESSURIZING. SHUT PACKS OFF FOR SEVERAL MINUTES. TURNED BACK ON WITH NO RETURN OF PRESSURIZATION. TROUBLESHOT IAW FIM 21-22-00-810-817. PERFORMED OPS TEST OF PRESSURE SWITCHES IAW 21-56-07-710-801. RT ENGINE PASSED. LT ENGINE FAILED. REPLACED LT ENGINE PRESSURE SWITCH. ALSO, PERFORMED SINGLE PACK CONFIDENCE CHECK ON BOTH PACKS . PERFORMED VERIFICATION FLT. INCLUDING 1 DERATED TO 33000FT. AND ONE MAX POWER T/O TO 17000 FT. PRESSURIZATION AND AIR CONDITIONING SYSTEMS CHECKED NORMAL.

Part: BRACKET — MISINSTALLED (GIRT BAR) · airframe 49,092 hrs · 26,037 cycles

DURING CHECK, AFT GIRT BAR BRACKET WAS INSTALLED BACKWARDS. MX RE-INSTALLED GIRT BAR BRACKET CORRECTLY.

Part: FLOOR SUPPORT — CORRODED (BS 1231-1269) · airframe 49,083 hrs · 26,029 cycles

AFT CARGO BAY, BS 1231-1269, FLOOR SUPPORT ANGLE ABOVE LONGERON 29R, CORRODED AROUND SEVERAL NUTPLATE HOLES. REPAIRED FLOOR SUPPORT IAW SRM 53-00-01 AND REINSTALLED IAW SRM 51-30-05.

Part: BEAM — CORRODED (BS 1250-1269) · airframe 49,083 hrs · 26,029 cycles

AFT CARGO BAY, MAIN BEAM L28R, CORRODED BETWEEN BS 1269-1250. BEAM FOUND TO BE OUT OF LIMITS. R & R BEAM IAW SRM 51-30-05 AND DWG 5730483 AT STA 1174-1307.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 49,083 hrs · 26,029 cycles

VERTICAL STABILIZER SKIN AT 1520 LONGERON 3R DAMAGED. ACCOMPLISHED REPAIR TO AFT FUSELAGE TO DORSAL FIN /SKATE ANGLE SPLICE IAW ERA 518618-14, REV O.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,083 hrs · 26,029 cycles

RIGHT STABILIZER L/E AT SPLICE BELT, INBD RIB IS CRACKED AT LIGHTNING HOLE. REPAIRED IAW ERA 519210, REV O.

Part: FRAME — CRACKED (BS 1520 BULKHEAD) · airframe 49,083 hrs · 26,029 cycles

INTERNAL TAIL EMPENNAGE AREA, NEAR TOP OF CANTED BULKHEAD FRAME BS 1520 JUST INBD OF STRINGER 3R FRAME ANGLE IS CRACKED. REPAIRED IAW ERA 517836-14, REV O AND PRI ERA 517836-14, REV 0, 1, 2.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 49,083 hrs · 26,029 cycles

FORWARD CARGO DOOR, FORWARD UPPER FOUR STOP FITTINGS CRACKED. R & R STOP FITTINGS IAW CMM 52-30-01.

Part: ATTACH ANGLE — BROKEN (VERTICAL-FUSE) · airframe 49,083 hrs · 26,029 cycles

THE RT FUSELAGE TO DORSAL FIN ATTACH ANGLE WAS CUT AT STA 1520, COMPLETELY SEVERED. OEM APPROVED REPAIR AS PERMANENT, ERA 518618-14. REQUIRES GVI AT 3000 CYCLES OR CHECK THRESHOLD.

Part: SKIN — CRACKED (BS 1531) · airframe 49,083 hrs · 26,029 cycles

AFT ACCESSORY COMPARTMENT, RT SIDE CANT FRAME BS 1531, FUSELAGE SKIN IS CRACKED. COMPLIED WITH PRI REV O, AND ERA 518608-14, REV A.

Part: SKIN — DAMAGED (NR 1 NACELLE) · airframe 49,083 hrs · 26,029 cycles

NR 1 PYLON LOWER SKIN WORN. REPAIRED IAW ERA 517820-14, REV O.

Part: SKIN — CORRODED (BS 1340-1347) · airframe 49,083 hrs · 26,029 cycles

AFT CARGO BAY, SKIN CORRODED, BS 1340-1347 BETWEEN L27-28R. ACCOMPLISHED ERA 517839-14, REV O.

Part: ATTACH ANGLE — CRACKED (BS 883) · airframe 49,083 hrs · 26,029 cycles

CENTER WING BOX UPPER SKIN, BS 883, XCW 48, LT CENTER TANK SKIN ATTACH ANGLE IS CRACKED. R & R DAMAGE IAW ERA 49819-14MA.

Part: SKIN — CRACKED (BS 1520) · airframe 49,136 hrs · 26,059 cycles

FUSELAGE AFT TAIL CONE AREA UPPER SKIN STRUCTURE, BS 1520, CANTED DOUBLER AND SKIN CRACKED AT LONGERON 3R. OEM APPROVED REPAIR AS PERMANENT, SECTION I COMPLETED IAW ER/A 517836-14.

Part: SPLICE — CORRODED (BS 1358 CHANNEL) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY BS 1358, L29L, CHANNEL SPLICE HAS CORROSION. R & R CHANNEL SPLICE IAW SRM 51-30-05, 53-10-01, AND 51-10-03.

Part: BEAM — CORRODED (BS 1212-1288) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO COMPARTMENT, STA 1212-1288, L29R BEAM IS CORRODED UNDER INTERCOSTAL. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED BEAM IAW SRM 53-00-01 AND 51-10-05 AND 51-30-05.

Part: STRUCTURE — CRACKED (BS 1542) · airframe 49,083 hrs · 26,029 cycles

AFT ACCESSORY COMPARTMENT, BS 1542, UPPER AFT CORNER OF LT VENT BOX IS CRACKED. R & R ANGLE SUPPORT IAW SRM 51-30-02, 51-30-05 AND 51-30-01.

Part: ATTACH ANGLE — CRACKED (BS 883) · airframe 49,083 hrs · 26,029 cycles

CENTER WING BOX, UPPER SKIN, BS 883, XCW 48, RT CENTER TANK, UPPER SKIN ATTACH ANGLE IS CRACKED. COMPLIED WITH PRI 518597-14, REV O AND ERA 518597-14, REV O AND ERA 498182-14MA.

Part: SKIN — CORRODED (BS 807-864) · airframe 49,083 hrs · 26,029 cycles

FORWARD RT WING TO BODY FAIRINGS BS 807-864, L26-29R HAS CORROSION ON SKIN. COMPLIED WITH PRI 518624-14 REV 0,1,2 AND ERA 518604-14, REV O.

Part: SHEAR TIE — CORRODED (BS 1288) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY BS 1288, L29-30R, SHEAR TIE IS CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-30-02.

Part: LONGERON — CORRODED (BS 1315-1355) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, LONGERON 30L CORRODED BETWEEN BS 1315 AND 1355. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED LONGERON. FABRICATED NEW AND INSTALLED IAW SRM 53-10-01.

Part: INTERCOSTAL — CORRODED (BS 1326-1344) · airframe 49,083 hrs · 26,029 cycles

AFT CARGO BAY, BS 1326-1344, L30 INTERCOSTAL HAS CORROSION ON UPPER AND LOWER FLANGES AND FORWARD TIE STRAP. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW INTERCOSTAL IAW SRM 51-30-05.

Part: LONGERON — CORRODED (BS 1390-1394) · airframe 49,083 hrs · 26,029 cycles

AFT CARGO BAY, LONGERON 27R CORRODED BETWEEN BS 1390 -1394. REMOVED LONGERON. LOCATED, DRILLED, TREATED, PRIMED, PAINTED AND INSTALLED NEW LONGERON IAW SRM 53-10-01, 51-10-05, & 51-10-03, 51-30-05.

Part: INTERCOSTAL — CORRODED (BS 1204-1212) · airframe 49,083 hrs · 26,029 cycles

AFT CARGO BAY, INTERCOSTAL CORRODED BETWEEN BS 1204 - 1212, L29 AND 30R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW INTERCOSTAL IAW SRM 51-30-02 AND 51-30-05.

Part: LONGERON — CORRODED (BS 1315-1364) · airframe 49,083 hrs · 26,029 cycles

AFT CARGO BAY, LONGERON L28R CORRODED BETWEEN BS 1315-1364. REMOVED CORROSION. LOCATED, DRILLED, TREATED, PRIMED, PAINTED AND INSTALLED LONGERON IAW SRM 51-10-05, 51-10-03, AND 51-30-05.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 49,082 hrs · 26,028 cycles

PASSENGER CABIN, FLOOR STRUCTURE, BS 200, RBL 57, BELOW U CHANNEL FOR R1 DOOR STRUCTURE IS CORRODED. COMPLIED WITH PRI AND ERA 518594-14, REV O.

Part: SHEAR TIE — CRACKED (BS 1458) · airframe 49,083 hrs · 26,029 cycles

AFT ACCESSORY BAY, LT SIDE BETWEEN LONGERONS 14 AND 15 LEFT, BS 1458, SHEAR TIE IS CRACKED AT UPPER FASTENER. REPLACED SHEARTIE IAW DWG 5913596 AND SRM 51-30-02, 51-30-05 AND 51-40-00.

Part: ANGLE — CORRODED (BS 1276) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, BS 1276, ANGLE AT FRAME AND OTBD SIDE OF 28R IS CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW ANGLE IAW SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (BS 1549) · airframe 49,082 hrs · 26,028 cycles

AFT ACCESSORY BAY, LT, BS 1549 CANTED FRAME, LOWER INTERCOSTAL IS CRACKED. R & R INTERCOSTAL AND REPAIR DOUBLER SPLICE IAW SRM 51-70-01, 51-00-01, 53-00-01 AND 51-10-03.

Part: FLOORBEAM — DAMAGED (BS 1060) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN LT FLOORBEAM AT STA 1060, LBL 48 HAS A DAMAGED HOLE. REMOVED DAMAGE AND REPAIRED IAW SRM 51-70-01.

Part: SKIN — CORRODED (BS 1354) · airframe 49,082 hrs · 26,028 cycles

ON REMOVAL OF LONGERON 27R, FOUND CORROSION ON INTERSKIN DOUBLER AT BS 1354. COMPLIED WITH ERA 517834-14, REV O AND PRI 517834-14, REV O AT STA 1354, L27R.

Part: SKIN — CORRODED (BS 1237-1250) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY DOOR CUT OUT, LOWER INNER SKIN, BETWEEN BS 1237 -1250, OUTSIDE OF S28R CORRODED. COMPLIED WITH ERA 517827-14, REV O AND PRI 517824-14 REV O.

Part: FRAME — CORRODED (BS 1344) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, BS 1344, BETWEEN L29L AND L27R, FORWARD FACE AND LOWER FLANGE OF FRAME IS CORRODED. FRAME FOUND TO BE OUT OF LIMITS. INSTALLED NEW FRAME ASSY IAW SRM 53-10-02.

Part: SHEAR TIE — CORRODED (BS 1276) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, SHEAR TIE, BS 1276, IS CORRODED BETWEEN L28 - 30R. REMOVED SHIEAR. LOCATED, DRILLED AND INSTALLED SHEAR TIE IAW SRM 51-30-02 AND 51-30-05.

Part: FRAME — CORRODED (BS 1307) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, LOWER AFT FLANGE OF FRAME, BS 1307 CORRODED BETWEEN L29L AND L29R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-10-02.

Part: SHEAR TIE — CORRODED (BS 1288) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, BS 1288, L29 - 30L, HAS EVIDENCE OF CORROSION BELOW SHEAR TIE. REMOVED CORROSION. 100 PERCENT MATERIAL LOSS. REPLACED SHEAR TIE IAW SRM 53-10-02.

Part: SHEAR TIE — CORRODED (BS 1288) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, BS 1288, L28 - 30R, AFT SIDE OF SHEAR TIES ARE CORRODED.. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SHEAR TIE IAW SRM 51-10-05 AND 51-30-02.

Part: LONGERON — CORRODED (BS 1354-1364) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, LONGERON L29R CORRODED BETWEEN BS 1354-1364. REPLACED LONGERON IAW SRM 51-30-05 AND 53-10-01.

Part: CUSP WEB — DAMAGED (BS 1060) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN BS 1060 CUSP WEB BETWEEN OTBD AND MIDDLE TRACKS HAS ELONGATED HOLES AT NUTPLATES. R & R IAW SRM 51-30-02 AND DWG 9940443, REV A.

Part: FRAME SPLICE — CORRODED (BSA 1328) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, AFT REPAIR SPLICE AT FRAME, BS 1328 CORRODED, BETWEEN 29L AND 29R. FABRICATED AND INSTALLED NEW SPLICE IAW SRM 53-10-02.

Part: SHEAR TIE — CORRODED (BS 1205) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY BS 1205, LONGERON 29L AND 29R, SHEAR TIE IS CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE IAW SRM 51-30-02 AND 51-30-05.

Part: FRAME — CORRODED (BS 1260) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY BS 1260, STUB FRAME, OTBD OF LONGERON 28R, HAS CORROSION ON FWD AND AFT SIDES. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, AND INSTALLED NEW STUB FRAME IAW SRM 51-10-05 AND 53-00-01.

Part: SEAT TRACK — CORRODED (BS 1180) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN COMPARTMENT, LT, BS 1180, OTBD SEAT TRACK UPPER SURFACE, IN TRACK, CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, 53-42-01 AND 53-20-01.

Part: SUPPORT ANGLE — CRACKED (BS 522) · airframe 49,082 hrs · 26,028 cycles

MID CARGO BAY BULKHEAD BS 522, RT SUPPORT ANGLE ABOVE LONGERON 28R IS CRACKED. R & R RT SUPPORT ANGLE IN MID CARGO COMPARTMENT. BULLKHEAD STA 522 IAW SRM 51-30-01 AND DWG 5936592-12, REV B.

Part: SHEAR TIE — CORRODED (BS 1250) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY BS 1250, SHEAR TIE IS CORRODED FROM LONGERON 29L-29R, 100 PERCENT MATERIAL LOSS. REPLACED SHEAR TIE IAW SRM 51-30-02 AND 53-00-01.

Part: FRAME — CORRODED (BS 1364) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY AFT SIDE OF FRAME, BS 1364 CORRODED, S26L- 29R. R & R SECTION OF FRAME IAW SRM 53-10-02.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 49,082 hrs · 26,028 cycles

FORWARD ENTRY DOOR, FIRST FRAME FROM TOP, AFT END ATTACH ANGLE IS CRACKED. REPAIRED IAW 27982-8000-0002.

Part: ANGLE — CORRODED · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, AFT SIDE OF APB WEB RT SIDE BACK-UP ANGLE FOR JACK POINT HAS CORROSION IN CORNER. COMPLIED WITH ERA 517823-14, REV O AND PRI 517823-14, REV O AT JACK POINT BACK UP ANGLE.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 49,082 hrs · 26,028 cycles

FORWARD ENTRY DOOR, UPPER CORNER IS CRACKED. REPAIR OF FORWARD ENTRY DOOR ACCOMPLISHED IAW 27985-8000-0003.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 49,082 hrs · 26,028 cycles

FORWARD ENTRY DOOR, FIRST FRAME FROM TOP, FORWARD END ATTACH ANGLE IS CRACKED. REPAIRED.

Part: SHEAR TIE — CORRODED (BS 1364) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, SHEAR TIE AT BS 1364, BETWEEN 28-29L, CORRODED. R & R SHEAR TIE IAW SRM 53-10-02.

Part: SHEAR TIE — CORRODED (BS 1364) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY, BS 1364, BETWEEN L28-29R FORWARD SIDE OF SHEAR TIE IS CORRODED. REPLACED SHEAR TIE SECTION.

Part: SHEAR TIE — CORRODED (BS 1364) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO COMPARTMENT, BS 1364, SHEAR TIE BETWEEN L30 AND L29L IS CORRODED ON FWD SIDE. REPLACED SHEAR TIE.

Part: CUSP WEB — CORRODED (BS 583) · airframe 49,082 hrs · 26,028 cycles

LEFT PASSENGER CABIN, CUSP WEB HAS CORRODED ON LOWER SURFACE, BS 583, LBL 57 AT LIGHTNING HOLE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW IAW SRM 53-00-01, 51-30-02 AND SMAL 2-13569.

Part: FRAME — GOUGED (BS 1437) · airframe 49,082 hrs · 26,028 cycles

TAIL COMPARTMENT LEFT SIDE FRAME AT BS 1437, JUST AFT OF TRIM AIR VALVE PREVIOUS REPAIR IS GOUGED. REMOVED GOUGE. DRILLED, TREATED, PRIMED AND INSTALLED NEW FILLER AND DOUBLER REPAIR IAW SRM 53-00-01, 51-30-00, 51-40-02, 51-10-31, 51-10-05.

Part: SEAT TRACK — CORRODED (BS 852-1136) · airframe 49,082 hrs · 26,028 cycles

RT PASSENGER CABIN, OTBD SEAT TRACK HAS NUMEROUS AREAS OF CORROSION ALONG ENTIRE UPPER SURFACE, BS 852-1136. BLENDED CORROSION. FOUND TO BE OUT LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, 51-10-03, AND 53-42-01.

Part: SEAT TRACK — CORRODED (BS 589-845) · airframe 49,082 hrs · 26,028 cycles

RT PASSENGER CABIN, OTBD SEAT TRACK HAS MULTIPLE AREAS OF CORROSION ALONG UPPER SURFACE, BS 589-845. FOUND OUT OF LIMITS IAW SRM 53-40-01. REMOVED, REPAIRED AND REINSTALLED SEAT TRACK IAW SRM 53-40-01.

Part: FRAME — CORRODED (BS 1240) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY STUB FRAME UNDER WEB, BS 1240, CORRODED. REMOVED STUB FRAME. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, AND INSTALLED FRAME IAW SRM 51-10-05 AND 51-30-05.

Part: FITTING — OUT OF LIMITS (GIRT BAR) · airframe 49,082 hrs · 26,028 cycles

FORWARD GALLEY & LAVATORY WET AREA, BS 171- 174, RBL 52 - 55. FOUND GIRT BAR FITTING OUT OF LIMITS IAW SRM 53-00-01. R & R GIRT BAR FITTING IAW SRM 51-30-01.

Part: FRAME — CORRODED (BS 1250) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY STUB FRAME UNDER WEB BS 1250, CORRODED. REMOVED CORROSION, 100 PERCENT MATERIAL LOSS. DRILLED IAW SRM 51-10-05. INSTALLED ON NRC 27980-1600/0013.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN, BS 560-579, RBL 60 CUSP WEB UPPER SURFACE HAS CORROSION. COMPLIED WITH ERA 517837-14, REV O AND PRI 517937-14, REV. O.

Part: SEAT TRACK — CORRODED (BS 1330-1336) · airframe 49,082 hrs · 26,028 cycles

RIGHT PASSENGER CABIN, OTBD SEAT TRACK HAS CORROSION ON UPPER SURFACE, BS 1330-1336. FOUND OUT OF LIMITS. REMOVED, REPAIRED, AND REINSTALLED SEAT TRACK IAW SRM 53-40-01.

Part: SEAT TRACK — CORRODED (BS 610-674) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN BS 610-674, OTBD SEAT TRACK UPPER SURFACE, CORRODED. REMOVED CORRODED SEAT TRACK FROM BS 540-850, LT OTBD. CORROSION OUT OF LIMITS. NEW SEAT TRACK FABRICATED AND INSTALLED IAW SRM 53-10-02.

Part: FRAME — CORRODED (BS 1220) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY STUB FRAME UNDER WEB BS 1220 CORRODED. REMOVED CORROSION, 100 PERCENT MATERIAL LOSS. LOCATED, DRILLED AND INSTALLED FRAME.

Part: FRAME — CORRODED (BS 1250) · airframe 49,082 hrs · 26,028 cycles

AFT CARGO BAY BS 1250, FRAME IS CORRODED ON LOWER FLANGE AFT SIDE OF FRAME ABOVE LONGERON 30. NEW STUB FRAME INSTALLED ON NRC 27980/1600/0013.

Part: FITTING — CORRODED (BS 195-198) · airframe 49,082 hrs · 26,028 cycles

FORWARD GALLEY & LAV WET AREA, BS 195-198, RBL 52-55, GIRT BAR FITTING HAS CORROSION ON UPPER SURFACE. FOUND FITTING TO BE OUT OF LIMITS. REPLACED GIRT IAW SRM 51-30-01.

Part: CUSP WEB — CORRODED (MAIN CABIN) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN, BS 522-2, RBL 60, CUSP WEB UPPER SURFACE HAS CORROSION. REPAIRED DAMAGED CUSP WEB IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (ZONE 200) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN, BS 598-3, RBL 60 CUSP WEB UPPER SURFACE HAS CORROSION AT FASTENER. FABRICATED AND INSTALLED CUSP WEB IAW ERA 397904-14.

Part: CUSP WEB — CORRODED (BS 636-641) · airframe 49,082 hrs · 26,028 cycles

LEFT PASSENGER CABIN CUSP WEB HAS CORROION ON UPPER AND LOWER SURFACE, BS 636-641, LBL 54-58. REMOVED CORROSION IAW SRM 53-20-02. FABRICATED CUSP WEB AND RING DOUBLERS IAW SRM 53-20-02.

Part: INTERCOSTAL — CRACKED (BS 1346-1363) · airframe 49,082 hrs · 26,028 cycles

AFT LAVATORY WET AREA, BS 1346 -1363, BL0, INTERCOSTAL IS CORRODED AND CRACKED AT NUTPLATE HOLES. R & R INTERCOSTAL IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (CABIN) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN, BS 541-7 TO 541, RBL 60, CUSP MEMBRANE UPPER SURFACE HAS CORROSION. REPAIRED DAMAGE CUSP WEB IAW SRM 53-20-02.

Part: FLOOR SUPPORT — CRACKED (BS 1346-1363) · airframe 49,082 hrs · 26,028 cycles

AFT LAV WET AREA, BS 1346 -1363, BL 0, FLOOR SUPPORT IS CORRODED AND CRACKED AT NUTPLATE HOLES. R & R FLOOR SUPPORT IAW SRM 51-30-02.

Part: CUSP WEB — CORRODED (BS 1174-1193) · airframe 49,082 hrs · 26,028 cycles

RIGHT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER AND LOWER SURFACE, BS 1174-1193, RBL 54-58. REMOVED DAMAGE AND REPAIRED RT PASSENGER CABIN CUSP WEB IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 956) · airframe 49,082 hrs · 26,028 cycles

LT PASSENGER CABIN, CUSP WEB HAS CORROSION ON LOWER SURFACE, BS 956, LBL 57. REMOVED CORROSION. FABRICATED AND INSTALLED NEW CUSP WEB IAW SMALL 243493 AND DWG 9940443.

Part: CUSP WEB — CORRODED (BS 889-896) · airframe 49,082 hrs · 26,028 cycles

RIGHT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER AND LOWER SURFACE, BS 889-896, RBL 56-58. REMOVED CORROSION. REPAIRED CUSB WEB IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 1066) · airframe 49,082 hrs · 26,028 cycles

LT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER AND LOWER SURFACE, BS 1066, LBL 57 AT LIGHTNING HOLE. CORROSION REMOVED AND FOUND OUT OF LIMITS. WORK ACCOMPLISHED ON NRC 27980/2400/0113.

Part: CUSP WEB — CORRODED (BS 237-256) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN, BS 237-256, RBL 60, CUSP WEB UPPER SURFACE HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION. REPAIRED CUSP WEB AND INSTALLED REPAIR IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 607-617) · airframe 49,082 hrs · 26,028 cycles

RT CABIN, CUSP WEB HAS CORROSION ON UPPER SURFACE, BS 607-617, RBL 54-58. REMOVED CORROSION. REMOVED, ALODINED, PRIMED AND INSTALLED CUSP WEB AND DOUBLER IAW SRM 51-10-03, 51-30-02 AND 53-20-02.

Part: CUSP WEB — CORRODED (BS 731-750) · airframe 49,082 hrs · 26,028 cycles

LT PASSENGER CABIN, CUSP WEB, HAS CORROSION ON LOWER SURFACE, BS 731-750, LBL 54-58. REMOVED CORROSION, REPAIRED CUSP WEB IAW SRM 53-20-02.

Part: SEAT TRACK — DAMAGED (BS 313) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN COMPARTMENT, LT, BS 313, LBL 56, OTBD SEAT TRACK INBD UPPER HOLE ELONGATED. REMOVED AND INSTALLED FABRICATED STRAP IAW SRM 53-40-01, 53-20-02, 51-30-01 AND 51-30-05.

Part: CUSP WEB — CORRODED (BS 237-256) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN, BS 237 - 256, RBL 60 CUSP WEB UPPER SURFACE HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION. REPAIRED AND INSTALLED CUSP WEB IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 1152) · airframe 49,082 hrs · 26,028 cycles

RT CABIN, CUSP WEB, HAS CORROSION ON UPPER SURFACE BS 1152, RBL 57, REMOVED CORROSION. FABRICATED CUSP WEB IAW SRM 53-20-02 AND DWG 9910151.

Part: CUSP WEB — CORRODED (BS 948-955) · airframe 49,082 hrs · 26,028 cycles

RT PASSENGER CABIN, CUSP WEB CORRODED, BS 948-955, RBL 56-58. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED CUSP WEB IAW SRM 53-20-02, FIG 11.

Part: CUSP WEB — CORRODED (BS 674-693) · airframe 49,082 hrs · 26,028 cycles

LT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER SURFACE, BS 674-693, LBL 54-58. REMOVED CORROSION IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 1122) · airframe 49,082 hrs · 26,028 cycles

RT PASSENGER CABIN, CUSP WEB CORRODED, BS 1122, RBL 57. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED WITH FILLER, DOUBLER AND RING DOUBLER, ALODINED AND PRIMED IAW SRM 53-00-01, 51-10-03, 51-30-05, 51-30-02.

Part: CUSP WEB — CORRODED (BS 750-756) · airframe 49,082 hrs · 26,028 cycles

RT PASSENGER CABIN, CUSP WEB CORRODED, BS 750-756, RBL 56-58. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED CUSP WEB IAW SRM 53-20-02, FIG 19.

Part: FLOOR SUPPORT — CORRODED (BS 1364-1403) · airframe 49,082 hrs · 26,028 cycles

AFT LAV WET AREA, BS 1364-1403, LBL 16 - 19, FLOOR SUPPORT IS CORRODED AND PROTECTIVE COATING IS CHAFED ON UPPER SURFACE. REMOVED CORROSION, FABRICATED , TREATED, PRIMED AND PAINTED REPAIR ANGLE IAW SRM 51-70-01.

Part: CUSP WEB — CORRODED (BS 765) · airframe 49,082 hrs · 26,028 cycles

LEFT PASSENGER CABIN, CUSP WEB CORRODED, BS 765, LBL 57. BLENDED CORROSION. REMOVED DAMAGED AREA. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 16.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 49,082 hrs · 26,028 cycles

PASSENGER CABIN CUSP WEB HAS CORRODED, BS 541-560, LBL 54-58. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 53-20-02, FIG 19 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 765) · airframe 49,082 hrs · 26,028 cycles

LT PASSENGER CABIN, CUSP WEB CORRODED, BS 765, LBL 57. BLENDED CORROSION. REMOVED DAMAGE. FABRICATED ALL REPAIR PARTS IAW SM 53-30-02 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 294-306) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN BS 294 - 306, RBL 60, CUSP WEB UPPER SURFACE HAS CORROSION. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 294-306) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN, BS 294-306, RBL 60, CUSP WEB CORRODED. R & R WEB IAW SRM 53-20-02, FIG 19.

Part: CUSP WEB — CORRODED (BS 569-572) · airframe 49,082 hrs · 26,028 cycles

PASSENGER CABIN, CUSP WEB, HAS CORROSION ON LOWER SURFACE, STA 560-572, LBL 54-58. REMOVED CORROSION. REPAIRED CUSP WEB IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 1255-1268) · airframe 49,082 hrs · 26,028 cycles

RIGHT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER SURFACE STA 1255-1268, RBL 54-58, TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 1136) · airframe 49,082 hrs · 26,028 cycles

LT PASSENGER CABIN, CUSP WEB HAS CORROSION AROUND FASTENER HOLE, STA 1136, LBL 49-50. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW PARTS IAW SRM 51-20-00 AND 51-30-02.

Part: CUSP WEB — CORRODED (BS 1255-1268) · airframe 49,082 hrs · 26,028 cycles

RIGHT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER SURFACE, BS 1255-1268, RBL 54-58. REMOVED CORROSION AND REPAIRED IAW SRM 53-20-02.

Part: CUSP WEB — CORRODED (BS 522-541) · airframe 49,082 hrs · 26,028 cycles

PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER AND LOWER SURFACE, STA 522-541, LBL 54-58. REMOVED CORROSION. NO PUBLISHED LIMITS. REPAIRED CUSP WEB IAW SRM 53-20-02, FIG 19.

Part: CUSP WEB — CRACKED (BS 226) · airframe 49,082 hrs · 26,028 cycles

PASSENGER CABIN LT CUSP MEMBRANE, STA 226, LBL 57, 2" CRACK AT LIGHTNING HOLE. REPAIRED IAW SRM 53-20-02, FIG 19.

Part: SEAT TRACK — CHAFED (BS 1364) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN LT, BS 1364, INBD SEAT TRACK UPPER SURFACE CHAFED. BLEND DAMAGE, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-40-01, PG 3 & 4, FIG 1.

Part: THRESHOLD — CORRODED · airframe 49,082 hrs · 26,028 cycles

AFT PRESSURE DOOR SURROUND STRUCTURE, THRESHOLD PLATE, HAS SEVERAL AREAS OF CORROSION ON UNDERSIDE THAT OVERLAPS UPPER STEP OF VENTRAL STAIR. REMOVED CORROSION. NDT FOUND TO BE OUT OF LIMITS. LOCATED , DRILLED, TOPCOATED AND INSTALLED NEW THRESHOLD IAW SRM 51-10-03, 51-30-01 AND DWG 5917579.

Part: CUSP WEB — CORRODED (BS 1231-1250) · airframe 49,082 hrs · 26,028 cycles

LT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER AND LOWER SURFACE, BS 1231-1250, LBL 54-58. TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-10-03 AND 53-20-02.

Part: SEAT TRACK — DAMAGED (BS 1310) · airframe 49,082 hrs · 26,028 cycles

MAIN CABIN COMPARTMENT, LT, BS 1310, CENTER SEAT TRACK OTBD HOLE ELONGATED AND NO EDGE DISTANCE. REMOVED DAMAGED SECTION OF SEAT TRACK AT STA 1308-1364, LBL 44. LOCATED, DRILLED, ALODINED, PRIMED, PAINTED AND INSTALLED NEW SEAT TRACK IAW SRM 53-20-01, 51-30-01, 53-40-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 49,082 hrs · 26,028 cycles

LEFT MLG RETRACT ACTUATOR SUPPORT FITTING INBD BUSHING BORE HAS MINOR CORROSION AT 6 O'CLOCK ON INBD END OF BORE. MACHINED LT MLG INBD BUSHING BORE TO REMOVE DAMAGE IAW DWG SR09570087. FOUND WITHIN LIMITS IAW SUBNOTE 11.

Part: CUSP WEB — CORRODED (BS 1116-1119) · airframe 49,082 hrs · 26,028 cycles

LEFT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER AND LOWER SURFACE, STA 1116-1119, LBL 55-57. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, PRIMED AND INSTALLED DOUBLER REPAIR IAW SRM 51-10-03, 53-20-02, AND PS 900-7-3 NR 3, PG 6, TABLE 1.

Part: FLOORBEAM — CRACKED (BS 218) · airframe 49,082 hrs · 26,028 cycles

FORWARD CABIN, BS 218, LBL 15 - RBL 15, FLOORBEAM CRACKED. REMOVED AND INSTALLED NEW FLOORBEAM IAW SRM 51-10-05, 51-30-02 AND DWG 4936535.

Part: CUSP WEB — CORRODED (BS 280-294) · airframe 49,082 hrs · 26,028 cycles

PASSENGER CABIN, LT CUSP MEMBRANE, BS 280-294, LBL 54-57 HAS CORROSION ON LOWER SURFACE, BETWEEN LIGHTNING HOLES. REPAIRED CORRODED CUSP WEB MEMBRANE AT ST 280-294, LBL 54-57 IAW SRM 53-20-02, PG 166, FIG 19.

Part: CUSP WEB — CORRODED (BS 617-637) · airframe 49,082 hrs · 26,028 cycles

RT PASSENGER CABIN, CUSP WEB HAS CORROSION ON UPPER SURFACE STA 617-637, RBL 54-58. TASK 53-211-02. REMOVED CORROSION. NDT FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED NEW REPAIR PART IAW 53-70-02, 51-10-03, 51-10-00 AND PSM 900-5-1, NR 04.

Part: SEAT TRACK — CORRODED (BS 704-706) · airframe 49,082 hrs · 26,028 cycles

RT INBD SEAT TRACK HAS CORROSION ON UPPER SURFACE BS 704-706. TASK 53-211-02. REMOVED CORROSION. NDT FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, TREATED, PRIMED AND INSTALLED PLUG REPAIR IAW SRM 51-10-03 AND 53-40-01.

Part: ATTACH ANGLE — CORRODED (BS 1363) · airframe 49,082 hrs · 26,028 cycles

AFT LAVATORY WET AREA, BS 1363, LBL 22, SEAT TRACK ATTACH ANGLE IS CORRODED. REMOVED SEAT TRACK, LOCATED, DRILLED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-10-05, 51-30-00.

Part: SEAT TRACK — CORRODED (BS 234) · airframe 49,082 hrs · 26,028 cycles

FORWARD GALLEY/LAVATORY WET AREA, BS 234, RBL 45, SEAT TRACK IS CORRODED ON INNER AND UPPER CROWN SURFACE. TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-30-01. 51-30-05.

Part: FLOORBEAM — CORRODED (BS 1364) · airframe 49,082 hrs · 26,028 cycles

AFT LAVATORY WET AREA, BS 1364, LBL 14- RBL 11, FLOORBEAM CORRODED ON UPPER SURFACE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOORBEAM IAW DWG 5930961, REV BL AND SRM 51-30-00.

Part: LONGERON — CORRODED (BS 168 L29L) · airframe 49,082 hrs · 26,028 cycles

E & E BAY, BS 168, LONGERON 29L CORRODED BY DOOR PAN. R & R LONGERON IAW SRM 51-30-02 AND 51-30-05.

Part: LONGERON — CORRODED (BS 168 L30L) · airframe 49,082 hrs · 26,028 cycles

E & E BAY, STA 168, LONGERON 30L CORRODED AT DOOR PAN AREA. R & R LONGERON IAW SRM 51-30-02 AND 51-30-05.

Part: LONGERON — CORRODED (BS 168 L29R) · airframe 49,082 hrs · 26,028 cycles

E&E BAY BS 168, LONGERON 29R CORRODED AT DOOR PAN. R & R LONGERON IAW SRM 51-30-02 AND 51-30-05.

Part: CATWALK — INOPERATIVE · airframe 48,632 hrs · 25,757 cycles

CREW REPORTED CATWALK WILL NOT STOW PROPERLY. REMOVED AND REPLACED DAMAGED LATCH ASSEMBLY PER AMM. REPOSITIONED CABLES. REMOVED AND INSTALLED CEILING ADJUSTMENT GUIDE AND VENTRAL STAIRWAY MOVEABLE CEILING. OPERATIONAL CHECKS GOOD. CREW REPORTED CATWALK WILL NOT STOW PROPERLY.

Part: LONGERON — CRACKED (BS 1458 L2L) · airframe 47,789 hrs · 25,255 cycles

LONGERON, BS 1458 L2L CRACKED. NO SRM REFERENCE FOR DAMAGE. ERA REMOVES DAMAGED SECTION OF LONGERON L2L HFEC INSPECTS TRIM LINE AND INSTALLES SPLICE IAW DWG SG90530003-7005.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,789 hrs · 25,255 cycles

SKIN BS 1475, JUST BELOW THE APU INLET DUCT ON THE RT SIDE, CRACKED. WORK COMPLIED WITH ON PRI/ERA 512045-14, REV O. HFEC AND INSTALLED REPAIR IAW SG90530003-7011 ZN80.

Part: STRINGER SPLICE — DAMAGED (BS 1475) · airframe 47,789 hrs · 25,255 cycles

STRINGER SPLICE DAMAGED BS 1475 S2L. REPAIRED IAW ERA 512143-14 SECTION II.

Part: SKATE ANGLE — CRACKED (VERTICAL STAB) · airframe 47,789 hrs · 25,255 cycles

LT ANGLE CRACKED, LOWER VERTICAL. REMOVED ANGLE FROM ACFT, DRILLED, AND INSTALLED SKATE ANGLE IAW DWG5912188 AND SRM 51-01.

Part: SHEAR TIE — DAMAGED (BS 1494) · airframe 47,789 hrs · 25,255 cycles

TIE CLIP SHEARED BS 1494, LBL 8 BETWEEN LONGERON 1 & 2 LEFT. REMOVED CRACKED SHEAR TIE CLIP, DRILLED NEW AND INSTALLED PER DWG9953016.

Part: SKIN — DAMAGED (BS 1475) · airframe 47,789 hrs · 25,255 cycles

ERA 512045-14, SECTION I, ISSUED FOR REPAIR TO BS 1475, L1-3R SKIN AND LONGERON AND SHEAR TIES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,701 hrs · 24,649 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: GROUND WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 45,877 hrs · 24,200 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY CEILING LIGHT INOPERATIVE RIGHT SIDE, ROW 14. RECONNECTED GROUND WIRE. OPERATION CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (TAILCONE) · airframe 45,248 hrs · 23,858 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THE TAIL CONE SIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AT AFT STAIRS PER AMM. OPERATION CHECKS GOOD.

Part: SENSOR — FAULTY (CABIN) · airframe 42,512 hrs · 22,574 cycles

CREW REPORTED THAT ON LANDING THEY HAD FUMES AND AN ODOR IN THE AFT CABIN. CABIN CREW AND SEVERAL PASSENGERS FAINT AND DIZZY. NOTED RT CABIN TEMPERATURE SUPPLY OCCASIONALLY FLUCTUATING TO 100 DEGREES ON CABIN TEMPERATURE INDICATOR. MX TROUBLESHOT IAW TSM 21-22 AND REPLACED CABIN TEMPERATURE SENSOR AND COALESCER BAGS. OPERATIONALLY TESTED IAW MM 21-62-04. CHECKS GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 42,329 hrs · 22,499 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 2 INOPERATIVE. MX FOUND BROKEN WIRE AND REPAIRED IT. FUNCTIONALLY CHECKED THE SYS.

Part: DUCT — DELAMINATED (THRUST REVERSER) · airframe 41,862 hrs · 22,311 cycles

RT ENGINE FIRE DET FAULT ON CLIMBOUT. RETURNED TO DEPARTURE, OVERWEIGHT LANDING. LOWER T/R C DUCT WAS FOUND DELAMINATED AND COMING APART IN THE COLD STREAM AREA. 7TH STAGE BLEED VALVE SOLENOID WAS REPLACED. LOWER COWL/ T/R ASSY WAS ALSO REPLACED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 41,093 hrs · 21,963 cycles

ACTION DURING LINE CHECK MX FOUND FIRST CLASS EMERGENCY LIGHTS WITH EXPOSED WIRES AND BROKEN. MX REPAIRED DAMAGED WIRES AND REPLACED LIGHTS. OPS CHECK OF LIGHTS NOW CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,646 hrs · 21,760 cycles

MX SET UP TO VERIFY ALL EMERGENCY LIGHTS AND SIGNS. MX FOUND EXIT SIGN AT L2 INOPERATIVE. SIGN WAS REPLACED AND OPS CHECK OF SIGN NOW OK.

Part: LIGHT — INOPERATIVE (ROW 35C) · airframe 40,252 hrs · 21,523 cycles

EMERGENCY FLOOR LIGHTING INOP AT 35C. REPLACED FLOOR TRACK LIGHT ASSY AND RED LENS. OPS CHECK OF LIGHT NOW OK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,782 hrs · 20,639 cycles

MAJOR REPAIR COMPLETED PER ERA 470350-14 REV B 8/18/09. LOCATED FUSELAGE STA 218 STR 18L.

Part: DOOR FRAME — CORRODED (FWD CARGO) · airframe 36,316 hrs · 19,179 cycles

FUSELAGE FORWARD CARGO DOOR LOWER FRAME, REPAIRED IAW ERA 470229-14, ERA 470229-14.

Part: PROXIMITY SENSOR — INTERMITTENT (RT MAIN GEAR) · airframe 34,136 hrs · 17,964 cycles

RT MAIN GEAR INDICATION INOP. GREEN INDICATION LIGHT CAME ON DURING TAXI ROLL OUT AFTER LANDING . SUSPECT DOWN LOCK PROX SENSOR. WILL UPDATE WHEN A/C BACK IN SERVICE. REPLACED RT GEAR DOWN/LOCK SENSOR. SWUNG GEAR SEVERAL TIMES. ALL CKS OK.

Part: PAN — CORRODED (CARGO DOOR FRAME) · airframe 33,576 hrs · 17,651 cycles

FWD PIT DOOR JAMB PAN OUT OF LIMITS STA 375 TO 422 (CORROSION). REPAIRED DOOR JAMB PAN IAW/MD-90 SRM 51-30-01, 51-30-02, 51-10-05, 53-05D FIG 804.

Part: SKIN — DENTED (BS 237 L18L) · airframe 33,576 hrs · 17,651 cycles

DENTED BELOW LONG 18L STA 237.8 DENT IS AT FRAME. REPAIRED IAW MD90 SRM 53-30-01 FIG 5.

Part: SKIN — DENTED (FS 1350 L26-28R) · airframe 33,576 hrs · 17,651 cycles

DURING HMV, DETN AND GOUGE DAMAGE WERE FOUND ON THE SKIN ADJACENT TO AN EXISTING REPAIR INSTALLED PER 365416-14. THIS REPAIR WAS REMOVED, THE ADDITIONAL DAMAGE WAS CUTOUT, AND A BOEING APPROVED REPAIR WAS INSTALLED PER 462740-14

Part: SKIN — CHAFED (LT WING) · airframe 33,576 hrs · 17,651 cycles

L WING L/E SKIN CHAFED 2 EA PLACES AT NR 5 SLAT TRACK. REPAIRED LT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL 1.

Part: ATTACH FITTING — CRACKED (BS 1079 L18R) · airframe 33,576 hrs · 17,651 cycles

FRAME FITTING RT FS 1079 UNDERSIDE OF CUSP (BELOW L18R) IS CRACKED. REMOVED AND INSTALLED NEW FRAME FITTING IAW SRM MD-90 51-30-5.

Part: DOOR FRAME — CORRODED (BS 685-757) · airframe 33,576 hrs · 17,651 cycles

MID PIT DOOR JAMB BEAM HAS CORROSION FROM FS 685 TO 757. REPAIRED MID PIT DOOR JAMB BEAM IAW MD80 SRM 53-05D.

Part: SEAT TRACK — GOUGED (BS 1150-1364) · airframe 33,576 hrs · 17,651 cycles

CABIN SEAT TRACK RBL 24 OUT OF LIMITS MULTIPLE AREAS FS 1150-1364 (REF 1002862 2700-0062). REPAIRED SEAT TRACK IAW MD-90 SRM 53-40-01 FIG 6 VOL I.

Part: LONGERON — CORRODED (BS 1364 L29L) · airframe 33,576 hrs · 17,651 cycles

AFT PIT LONGERON 29L IS CORRODED AT STA 1364. REPLACED LONGERON 29L IAW MD90 SRM 51-30-05 AND 51-30-02.

Part: CUSP WEB — CORRODED (BS 676-746) · airframe 33,576 hrs · 17,651 cycles

RT CUSP WEB CORRODED OUT OF LIMITS FS 676-746. REPAIRED CUSP WEB IAW EA 398191-14MA DATED 9/18/02.

Part: CUSP WEB — CORRODED (BS 1080) · airframe 33,576 hrs · 17,651 cycles

RT CUSP WEB CORRODED OUT OF LIMITS FS 1080, TRIMMED OFF DAMAGED CUSP SECTION FABRICATED NEW AND INSTALLED IAW DAL ERA 398191-14MA, MD90 SRM 51-30-02, 51-30-01, 51-30-05 AND 51-10-03.

Part: CUSP WEB — CORRODED (BS 1080) · airframe 33,576 hrs · 17,651 cycles

RT CUSP WEB CORRODED OUT OF LIMITS FS 1080. TRIMMED OFF DAMAGED CUSP WEB SECTION, FABRICATED NEW, AND INSTALLED IAW EA 398191-14MA, MD-90 SRM 51-30-02, 51-30-01, 51-30-05 AND 51-10-03 ON NR 2700-0172 AT HMV-2 IN OKC.

Part: CUSP WEB — CORRODED (BS 530) · airframe 33,576 hrs · 17,651 cycles

RT CUSP WEB CORRODED OUT OF LIMITS O/B EDGE FS 530. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW MD-80 53-05D.

Part: HINGE — CORRODED (HORIZONTAL STAB) · airframe 33,576 hrs · 17,651 cycles

VERT TO HORZ STAB LT I/B HINGE PLATE HAS PITTING AND CORROSION ON O/B SURFACE AND IN BORES. REPAIRED IAW MD-90 SRM 55-30-05 PARA 5

Part: HINGE — CORRODED (HORIZONTAL STAB) · airframe 33,576 hrs · 17,651 cycles

VERTICAL TO HORIZONTAL STAB RT I/B HINGE PLATE HAS PITTING CORROSION IN BORES. REMOVED CORROSION AND INSTALLED REPAIR BUSHINGS IAW MD90 SRM51-30-05 AND 55-30-05 PARA 5.

Part: HINGE — CORRODED (HORIZONTAL STAB) · airframe 33,576 hrs · 17,651 cycles

LT O/B HINGE PLATE HAS CORROSION ON I/B AND O/B SURFACE AND LIGHT FRETTING IN BORES. REPAIRED IAW MD-90 SRM 55-30-05 PARA 5.

Part: HINGE — CORRODED (VERTICAL STAB) · airframe 33,576 hrs · 17,651 cycles

VERT TO HORIZ STAB RT O/B HINGE PLATES HAS CORROSION ON I/B AND O/B SURFACES AND PITTING CORROSION IN BORES. REPAIRED RT O/B HINGE PLATE IAW MD-90 SRM 55-30-05 PARA 5.

Part: CUSP WEB — CORRODED (BS 773) · airframe 33,576 hrs · 17,651 cycles

LT CUSP WEB OUT OF LIMITS AT LIGHTING HOLE FS 773. REPAIRED CUSP WEB IAW MD88 SRM 53-05D FIG 827D.

Part: CUSP WEB — CRACKED (BS 873) · airframe 33,576 hrs · 17,651 cycles

LT CUSP WEB OUT OF LIMITS, CRACKED AT LIGHTEN HOLE FS 873. REPAIRED CUSP WEB IAW MD-88 SRM 53-05D FIG 827D.

Part: CUSP WEB — CORRODED (BS 1212-1269) · airframe 33,576 hrs · 17,651 cycles

AFT CUSP WEB STA 1212-1269 RT CORRODED 3 EA PLACES 1269,1240,1216. REPAIRED CUSP WEB AT STA 1240 RT SIDE IAW DELTA ERA 398191-14MA REV A 9/18/02

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,576 hrs · 17,651 cycles

CUSP WEB IS CORRODED UNDER L-2 GIRT BAR FITTING. CUT OUT DAMAGED AREAS REPAIRED IAW ERA 39819-14MA REV ORG 9/18/02.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 33,576 hrs · 17,651 cycles

AFT PIT DOOR CUT OUT LOWER BEAM CORRODED ON VERTICAL AND HORIZONTAL FLANGE. REPAIRED AFT PIT DOOR CUT OUT LOWER BEAM IAW MD-80 SRM 53-05D FIG 63 AND SRM 51-00-01 PG 2 MD90.

Part: SEAT TRACK — CORRODED (BS 1212-1304) · airframe 33,576 hrs · 17,651 cycles

FOUND SEAT TRACK LBL 54 FS 1212 TO 1304 EXFOLIATED CORROSION. REMOVED DAMAGED SEAT TRACK AND REPLACED WITH NEW IAW MD-90 SRM 51-30-05, 51-30-1, 51-10-05, 53-40-01 AND 51-10-03.

Part: CUSP WEB — CRACKED (BS 1344) · airframe 33,576 hrs · 17,651 cycles

CRACK IN FLOOR WEB LEFT CUSP WEB AT LT FUSELAGE STA 1344 UNDER GALLEY. REPAIRED CUSP WEB IAW DELTA ERA 413196-14MA REV ORG 05/15/03.

Part: SKIN — DENTED (BS 218 L18L) · airframe 33,576 hrs · 17,651 cycles

DENT BELOW LONGERON 18L AT STA 218, DENT IS AT A FRAME. REPAIRED IAW MD-80 SRM 53-04D FIG 12B, MD-90 SRM 51-00-01 PG 2 ID REPAIR IAW DAL PROCESS STANDARD 900-5-1 NO 4.

Part: SEAT TRACK — CORRODED (BS 1148-1180) · airframe 33,576 hrs · 17,651 cycles

FOUND CABIN SEAT TRACK LBL-54 OUT OF LIMITS STA 1148-1180. REPLACED SEAT TRACK AT LBL-54 STA 1088-1193 IAW MD-90 SRM 51-30-1.

Part: BOLT — BROKEN (RT HORZ STAB) · airframe 32,422 hrs · 17,002 cycles

RT MANUAL REVERSION CYLINDER HOUSING BOLTS BROKE AND THE HOUSING BODY CAME APART CAUSING BOTH HYDRAULIC SYSTEMS TO LOSE QUANTITY. THIS RESULTED IN LOSS OF STEERING AND BRAKING DURING TAXI TO GATE AFTER LANDING. AIRCRAFT WAS MET ON THE TAXIWAY AND TOWED TO THE GATE BY MAINTENANCE. REMOVED RT REVERSION CYL 453597. INSTALLED MANUAL REVERSION ACTUATOR PER MM 27-33-09-420-801 TO STEP G 223122. OPS CK LEAK FUNCTIONAL RTS PER MMR. INSP C/W QC50.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 30,650 hrs · 16,029 cycles

NORMAL LANDING AT DEN WITH NORM SPEED LT REVERSER ON MCO, MED AUTOBRAKES. TURNING INTO GATE GOT HOT BRAKES. TEMP OFF SCALE. FUSE PLUGS BLEW AND TIRES DEFLATED. REPORTED BRAKE FIRE. REPLACED NR 1 AND 2 BRAKES. REPLACED NR 1 AND 2 MAIN WHEELS ASSY PER MM. REMOVED BOTH 1 AND 2 TIRES FOR GEAR INSP. REINSTALLED BOTH 1 AND 2 BRAKES AND WHEEL ASSYS PER MM.

Part: GENERATOR — FAILED (NR 2 ENGINE) · airframe 30,137 hrs · 15,742 cycles

RIGHT GEN INOP ON MCO, APU LOW ON OIL, MSG IN FLIGHT. RETURN TO GATE. REPLACED RIGHT GEN, CHECKS GOOD. SERVICED APU, CHECKS GOOD. NO LEAKS.

Part: DUCT — FAILED (LT A/C PACK) · airframe 29,731 hrs · 15,540 cycles

ON CLIMBOUT AT 6000 FT FLOW LIGHT ILLUMINATED. AT ALTITUDE OF 10000 (CABIN ALT 9000) FLOW LIGHT WENT OUT. WHEN CLIMB INITIATED FLOW LIGHT CAME ON AGAIN AND CABIN ALT WARNING SOUNDED. FLT ATTENDANT REPORTED LOUD NOISE FROM AROUND 2 L DOOR AREA. REPLACED BLOWN DUCT BOOT FROM LEFT PACK OUTLET.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 25,531 hrs · 13,401 cycles

ACS REPORTED TAIL PIPE FIRE NR 2 ENGINE AFTER ENGINE SHUTDOWN. REPLACED ENGINE.

Part: GENERATOR — CRACKED (NR 2 ENGINE) · airframe 23,423 hrs · 12,352 cycles

ON TAKEOFF ROLL PILOT ABORTED TAKEOFF WHEN HE GOT A RT GEN OVERHEAT MESSAGE AND A RT GEN FILTER MESSAGE. REPLACED VSCF FOR CRACKED HOUSING

Part: SENSOR — FAILED (RT ELEVATOR) · airframe 22,089 hrs · 11,669 cycles

AT CRUISE FL330 EOAP MESSAGE ELEVATOR SPLIT & PYLON FLAP FAULT ILLUMINATED. ALSO NO AUTOLAND ILLUMINATED ON FMA. RAN RTS ON DFGC 1 & 2. GO ON BOTH. RAN ACS TEST. NO FAULTS FOUND ELEVATOR POSITION SENSOR NR 2 ON DFGC 2. REPLACED RT ELEVATOR POSITION SENSOR IAW AMM 27-34-01-5.

Part: ENGINE — POWER LOSS (NR 1) · airframe 20,775 hrs · 11,016 cycles

LEFT ENGINE POWER ROLLED BACK AND EGT 625. CREW FOLLOWED POM AND SHUT ENGINE DOWN. REPLACED NR 1 ENG PER M/M.

Part: ENGINE — OVERTEMP (NR 1) · airframe 20,772 hrs · 11,015 cycles

ON CLIMBOUT EGT ROSE PAST RED LINE AFTER THROTTLE RETARDED TO DECREASE EGT. ENG AUTO SHUTDOWN. REPLACED ENG DUE TO EGT EXCEEDANCE.

Part: OVEN — DIRTY (GALLEY) · airframe 20,464 hrs · 10,861 cycles

FWD JUMPSEAT HALON EXTINGUISHER USED IN FWD GALLEY OVEN DUE TO A SMOLERING PIECE OF PAPER. CLEANED OVEN AND REPLACED HALON EXTINGUISHER.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 18,266 hrs · 9,761 cycles

AIRCRAFT DIVERTED TO LUBBOCK TX WITH PUNGENT ELECTRICAL/PLASTIC SMELL IN COCKPIT. REPLACED WX RADAR INDICATOR FOR PRODUCING SMELL.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,654 hrs · 8,896 cycles

A/C 9201 IN DFW FOR E-2 CHECK FOUND CORROSION ON O/B FLOOR SEAT TRACK DIRECTLY BELOW AFT GALLEY MOUNT FOR G-2 GALLEY. REPAIRED SAME.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 16,072 hrs · 8,600 cycles

LEFT ENGINE ROLLBACK AND ABORTED TAKEOFF AT 70 TO 80 KNOTS. FOUND FAULT IN EEC. REPLACED NR 1 ENG EEC. RAN ENG PER PFHB, OP CKS GOOD.

Part: LINE — LEAKING (HYDRAULIC SYSTEM) · airframe 15,091 hrs · 8,072 cycles

RT HYDRAULIC SYSTEM FAILURE. GROUND SERVICE PRESSURE LINE IN RT WHEEL WELL LEAKING. LINE PREVIOUSLY ON MCO AND TEMP REPAIR ACCOMPLISHED. REPLACED WITH TEMPORARY FLEX LINE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 15,017 hrs · 8,031 cycles

THE LOWER SILL BEAM OF THE C3 CARGO DOOR SURROUND STRUCTURE WAS FOUND WITH SEVERAL AREAS OF CORROSION ON THE O/B SKIN FLANGE FROM FS 1244 - FS 1258. THE CORROSION WAS BLENDED AWAY WITH LESS THAN 20 PERCENT MATERIAL REMOVAL AT ANY LOCATION. THE AREA WAS TREATED FOR CORROSION PREVENTION. THE REPAIR IS THE SAME AS MD-88 SRM 53-05, FIG 63 AND IS ACCOMPLISHED PER ER/A 377798-14.

Part: BATTERY — INOPERATIVE (BATTERY BAY) · airframe 14,477 hrs · 7,749 cycles

BATTERY BUS OFF LIGHT ILLUMINATED INFLIGHT. REPLACED BATTERIES AND CHARGER.

Part: BRAKE — DRAGGING (NR 1)

AFTER TAKEOFF, LEFT OUTBOARD BRAKE TEMP REACHED 700 DEG. EXTENDED GEAR AND BRAKE COOLED TO 400 DEG. THEN RETRACTED GEAR FOLLOWED POM PROCEDURES. REPLACED BOTH NR 1 AND NR 2 MAIN WHEEL ASSY PER M/M DUE TO NR 1 MAIN FLAT WHEN REACHING GATE. ALSO, CHANGED NR 1 BRAKE ASSY PER M/M LEAK CHECKS GOOD.

Part: CONVERTOR — FAILED (LEFT)

L AC PWR FAULT AND L GEN OFF MSG ON OAP. APU IS ON MCO/PLAC. PER EPCU BITE, REPLACED LEFT A/C CONVERTER. OPS CKS NORMAL.

Part: SKIN — DENTED (BS 1353)

THE FUSLEAGE SKIN AT FS 1353 WAS DENTED AND CREASED BETWEEN STRINGERS 28L AND 28R. STRINGER 29L WAS ALSO DENTED. THE SKIN DAMAGE WAS REMOVED WITH A 18.75 X 20.75 CUTOUT AND A 4 INCH SECTION OF THE DAMAGED STRINGER WAS REMOVED. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE MD-90SRM (CLASS 2 REPAIR) AND THE STRINGER WAS SPLICED WITH PER THE MD-90 SRM. THE REPAIR WAS DOCUMENTED PER ER/A 365416-14.

Part: ANGLE — CRACKED (BS 937)

FUSELAGE/ATTACH FITTING, VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE: REPAIR FOR CRACK. THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE ON THE LT SIDE OF THE AIRCRAFT WAS FOUND WITH A .90 CRACK AT FS 937. THE CRACKED FLANGE WAS TRIMMED OUT AND A .080 THICK A-286 STEEL REPAIR ANGLE WAS INSTALLED PER ER/A 364553-14.

Part: CONVERTER — FAILED (LEFT)

LT AC PWR FAULT, LAC BUS OFF, DC BUS OFF. DURING CRUISE LOST ALL LT AC PWR AND LT AC ELECTRICAL FUNCTIONS. AFTER LDG APU GEN PICKED UP LT ELECTRICAL LOAD BUT STILL HAD LT AC PWR FAULT MSG. DIVERTED ABQ. RAN ALL ENGS AND APU, GEN AND CROSSTIE FUNCTIONS OPN NML. PERFORMED BITE ON EPCU, LT CONVERTER FAULT FOR LAST 5 LEGS. REPLACED LT CONVERTER. GEN AND CROSSTIE SYS CKS NML.

Part: SENSE LINE — LOOSE (NR 1 ENGINE)

SHORTLY AFTER T/O, AIRCRAFT LOST BOTH A/C PACKS. CABIN ALT CLIMBED, NO PNU FROM NR 1 ENG. THE AUTO PACK TRIP TRIPPED BOTH PACKS. FOUND SENSE LINE TO 10TH STAGE VALVE BACKED OFF. REINSTALLED LINE.

Part: FIRE LOOP MOUNT — LOOSE (NR 1 ENGINE)

A-LOOP FIRE DETECTOR LT ENG ILLUMINATED IN-FLIGHT DURING DESCENT TO DFW. B-LOOP ALREADY ON MCO. CORRECTIVE ACTION: FOUND MOUNT PLATE FOR A/B LOOPS LOOSE. SECURED SAME. A-LOOP TEST GOOD. ALSO, REPAIRED BAD WIRE AT LOOP CANNON PLUG. A/B LOOPS NOW TEST NORMAL.

Part: BRAKE — FAILED (NR 2)

NR 1 ENGINE FOD DAMAGE TO 1ST STAGE BLADES DUE TO NR 2 BRAKE FAILURE.