N927DN

Part: CABLE — FRAYED (TAILCONE) · airframe 45,844 hrs · 30,054 cycles

DURING OPERATIONAL CHECK OF AFT ENTRY DOOR TAILCONE EMERGENCY RELEASE MECHANISM FOUND BALL CABLE ASSEMBLY FRAYED. REMOVED AND REPLACED CABLE AND ADJUSTED PER AMM53-52-01. OK FOR SERVICE.

Part: GAUGE — DEFECTIVE (TAILCONE) · airframe 45,844 hrs · 30,054 cycles

DURING DEPRESSURIZING THE TAILCONE DISPLACEMENT SYSTEM NITROGEN BOTTLE FOUND WATER IN THE GAGE. INSTALLED NEW GAUGE.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 44,095 hrs · 29,025 cycles

NOTICED CORROSION AROUND HORIZONTAL STAB BARREL NUT. REMOVED THE BOLT AND BARREL NUT. MACHINED LOWER FORWARD SPAR CAP BARREL NUT HOLES TO REMOVE DAMAGE BEYOND LIMITS OF SRM 55-10-03. COMPLY WITH PRI/ERA 564200-14.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,963 hrs · 28,351 cycles

BATTERY POWER SUPPLY BS-229 INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY. OPERATION CHECKS GOOD.

Part: LONGERON — CORRODED (BS 1207-1268) · airframe 42,933 hrs · 28,333 cycles

CORROSION ON LONGERON 29R, BS 1207-1268. REPAIRED IAW ERA 558153-14 AND ETI 90-17-053.

Part: SKIN — CRACKED (BS 1475) · airframe 42,931 hrs · 28,332 cycles

CRACKED INNER FUSELAGE SKIN, BS 1475 BETWEEN LONGERONS 1 & 2R. REPAIRED IAW ERA 558142-14.

Part: PIN — OUT OF POSITION (R1 DOOR SLIDE) · airframe 42,931 hrs · 28,332 cycles

PIN ON R1 DOOR SLIDE OUT OF POSITION. REMOVED AND REPLACED SLIDE IAW MM.

Part: CABLE — BROKEN (DOOR SLIDE) · airframe 42,931 hrs · 28,332 cycles

BROKEN CABLES ON SLIDE LANYARDS OF L1, R1, AND L2 DOORS. NEW LANYARDS INSTALLED IAW MM. (LP# 0076898)

Part: BEAM — CORRODED (BS 693-750) · airframe 42,931 hrs · 28,332 cycles

CORROSION MID CARGO COMPARTMENT LOWER DOOR FRAME BEAM BETWEEN BS 693 - 750. REPAIRED IAW ERA 558143-14 AND ETI-90-17-051 R5.

Part: FRAME — CRACKED (BS 924) · airframe 42,931 hrs · 28,332 cycles

CRACK ON UPPER RADIUS OF FRAME TAB OF LEFT OVERWING FRAME, BS 924. REPLACED IAW SRM 51-30-01, 51-30-02, 51-30-05 AND DWG SR90530027, REV A.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 42,931 hrs · 28,332 cycles

CRACKED RIGHT HAND INNER DORSAL FIN JOINT ANGLE STA 1478-1468. REPLACED IAW SRM 51-30-05 AND 51-30-02.

Part: FRAME — CRACKED (BS 924) · airframe 42,931 hrs · 28,332 cycles

CRACK ON UPPER RADIUS OF FRAME TAB OF THE LEFT OVERWING FRAME BS 924. REPLACED IAW DWG SR90530027, REV A, AND 51-30-01, 51-30-02, 51-30-05.

Part: SKIN — NOT REPORTED (BS 1250-1542) · airframe 42,931 hrs · 28,332 cycles

FUSELAGE SKIN BETWEEN LONGERON 27L AND 25L, BS 1520 TO 1542. REPAIRED IAW ETA 90-17-040, AND ERA 558116-14, REV O.

Part: FRAME ANGLE — CRACKED (BS 1486) · airframe 42,931 hrs · 28,332 cycles

CRACKED FRAME ANGLE AT BS 1486 BETWEEN LONGERONS 2R - 3R IN THE AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-30-05 AND DWG 9953016.

Part: ANGLE — CRACKED (BS 1460) · airframe 42,931 hrs · 28,332 cycles

CRACKED LEFT DORSAL FIN JOINT ANGLE BS 1460. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.

Part: SKIN — WORN (L1 DOOR) · airframe 42,931 hrs · 28,332 cycles

WEAR ON L1 DOOR EXTERNAL SKIN AT GUST LOCK CUTOUT. REPAIRED IAW ERA 558134-14 AND ETI 90-17-047.

Part: WEB — CORRODED (BS 370-427) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FORWARD CARGO BAY WEB BETWEEN BS 370 - 427, LONGERON 24 AND 28R. REPAIRED IAW ETI90-17-046 AND ERA 558134-14, REV A.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 42,931 hrs · 28,332 cycles

ELONGATED HOLES ON THE FUEL TANK ACCESS PANEL 620EB. THE ACCESS PANEL WAS REPLACED.

Part: STRAP — CORRODED (BS 1231-1328) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON STRAP BELOW LONGERON 26L, BS 1231-1328, IN THE AFT CARGO BAY. REPLACED THE STRAP IAW DWG 5936021, REV EH.

Part: STRAP — CORRODED (BS 693-740) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON STRAP OF ANCHOR NUTS BETWEEN BS 693 - 703 AND 731 - 740 INSIDE THE MID CARGO DOOR FRAMEWEB. REPLACED IAW SRM 51-30-02 AND DWG 5930481.

Part: SUPPORT — CORRODED (BS 1212-1269) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON SUPPORTS BS 1212 AND 1269 FORWARD AND AFT LOWER CORNER FRONT OF DOOR FRAME BEAM IN THE AFT CARGO BAY. REPLACED THE SUPPORT IAW SRM 51-30-05.

Part: CARGO TRACK — CORRODED (BS 1269-1307) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON RIGHT CARGO TRACK BS 1269 - 1307 IN THE AFT CARGO BAY. REPLACED THE CARGO TRACK IAW SRM 51-30-01.

Part: STRAP — CORRODED (BS 1202-1279) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON SEVERAL ANCHOR NUT STRAPS BETWEEN BS 1202 - 1279 BETWEEN LONGERONS 27 - 29R INSIDE OF THE DOOR FRAME WEB IN THE AFT CARGO BAY. REPLACED IAW SRM 51-30-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FUEL ACCESS PANEL 520AT. REPLACED IAW MM.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FUEL ACCESS PANEL PANEL 520AT. REPLACED THE ACCESS PANEL.

Part: INTERCOSTAL — CORRODED (BS 826-845) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON INTERCOSTAL, RIGHT & LEFT HAND SIDE UNDER TIE TRACK BS 826 - 845. REPLACED IAW SRM 51-30-01, 51-30-02 AND 51-30-05.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 620CT, LEFT WING. REPLACED THE ACCESS PANEL.

Part: STRAP — CORRODED (BS 693-740) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON STRAP OF ANCHOR NUTS BETWEEN BS 693 - 702 AND 731 - 740 AT THE MID CARGO DOOR FRAME WEB. REPLACED THE STRAP IAW SRM 51-30-02 AND DWG 5930481, REV AE.

Part: DOOR FRAME — CRACKED (LT OVERWING DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACK ON UPPER RADIUS OF FRAME TAB LEFT OVERWING FRAME BS 924. REPLACED IAW DWG SR90530027, REV A, SRM 51-30-01, 51-30-02 AND 51-30-05.

Part: FLANGE — CRACKED (BS 275) · airframe 42,931 hrs · 28,332 cycles

CRACK ON THE LOWER FLANGE OF THE EQUIPMENT COOLING EXHAUST, LEFT SIDE OF FUSELAGE AFT OF BS 275. REPAIRED IAW ERA 464964-14, REV MA.

Part: RUB STRIP — CORRODED (RT WING) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON RUB STRIP FUEL PANELS 620CB, 620DB, 620EB, 620GB, 620HB, 620JB, 620LB, 620MB, 620PB AND RIGHT HAND FUEL MAIN TANK. REPLACED RUB STRIPS IAW SRM 57-10-05.

Part: SKIN PANEL — DAMAGED (HORIZ STAB) · airframe 42,931 hrs · 28,332 cycles

DAMAGED AREA HORIZONTAL STABILIZER UPPER AFT SKIN PANEL. REPAIRED IAW SR90550000, REV B.

Part: SKIN PANEL — CRACKED (RT HORIZ STAB) · airframe 42,931 hrs · 28,332 cycles

CRACK ON UPPER AFT SKIN PANEL AT RIGHT HAND HORIZONTAL STABILIZER. REPAIRED IAW DR90550000, REV B.

Part: RUB STRIP — CORRODED (WING) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON RUB STRIP ON FUEL PANEL 620AT, 620CT, 620DT AND 620FT. FOUND TO BE OUT OF LIMITS. REPLACED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACKED FUSELAGE SKIN ON LEFT HAND AFT NOSE LANDING GEAR AFT HINGE. REPAIRED IAW SRM 53-03-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON INTERCOSTAL STA 1288-1309 AND 1322-1344 LONGERON 30. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 936071.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON INTERCOSTAL STA 1269-1288 LONGERON 30 AND 29L AFT CARGO COMPARTMENT. REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5936071.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON PRODUCTION SPLICE STA 1240 BETWEEN 27L-29R AFT CARGO COMPARTMENT. REPLACED IAW SRM 51-30-05, 51-30-02 AND DWG 5936667.

Part: BEAM — CRACKED (R1 DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACK ON THE R1 DOOR BEAM NR 4 FORWARD EDGE. REPLACED IAW SRM 51-30-02, 51-30-05, AND DWG 9911582, REV T.

Part: HINGE FITTING — CORRODED (VERTICAL STAB) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON INBOARD LUG BORE AT LEFT VERTICAL STABILIZER HINGE FITTING. REPAIRED IAW SRM 55-30-05.

Part: INTERCOSTAL — CRACKED · airframe 42,931 hrs · 28,332 cycles

CRACK ON INTERCOSTAL BETWEEN BEAMS NR 4 AND 5 AT L1 DOOR. REPLACED IAW SRM 51-30-01, 51-30-02, AND DWG 9955763, REV M.

Part: ANGLE — CORRODED (BS 1402-1443) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON ANGLES AND SUPPORTS BETWEEN BS 1402 - 1443, LONGERONS 28 TO 29R AND 28 - 29L. REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACK AND DISBANDED ON FUSELAGE INNER SKIN DOUBLER PREVIOUS REPAIR STA 237 LONGERON 17L. REPAIRED IAW SRM 53-31-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FUEL ACCESS PANEL 620DT. REPLACED THE ACCESS PANEL.

Part: RUB STRIP — CORRODED (ACCESS PANELS) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON RUB STRIPS ON CUTOUT FUEL ACCESS PANELS 520CT, 520AT, 520DT AND 520F. REPLACED IAW SRM 57-10-05.

Part: HINGE FITTING — DAMAGED (HORIZONTAL STAB) · airframe 42,931 hrs · 28,332 cycles

ELONGATED HOLE OF SIDE OF LEFT HINGE FITTING ON REAR SPAR BETWEEN XH 7.234 AND XHS 14.649 RIGHT HORIZONTAL STABILIZER. REPLACED IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (BS 674-760) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON CUSP WEB UPPER & LOWER SURFACES BETWEEN RBL 54 TO 60, BS 674 - 760. FABRICATED AND INSTALLED A NEW CUSP WEB IAW SRM 53-20-02.

Part: BEAM — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACKED LEFT HAND DOOR JAMB BEAM ON NLG STA 41-69. REPAIRED IAW SRM 53-90-01.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACKED PERVIOUS REPAIR DOUBLER ON FRAME STA 1542 CANT AND RIGHT HAND VENTRAL STAIRWAY DOOR JAMB. REPLACED DOUBLER IAW SRM 51-30-02 AND 51-30-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON RIGHT HAND CUSP WEB BETWEEN STA 1245-1247 AND 1255-1257, X=-54 TO -60. REPAIRED IAW SRM 53-20-02.

Part: BAR — WORN (L2 DOOR) · airframe 42,931 hrs · 28,332 cycles

WEAR ON BAR AT L2 DOOR BETWEEN LOWER AND UPPER HINGES. REPAIRED IAW ERA 530703-14MA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FLOOR FITTINGS BETWEEN STA 160-200, X=-54. REPLACED FLOOR FITTINGS IAW DWG 9936534-REV BW.

Part: RUB STRIP — CORRODED (WING) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON RUB STRIPS ON ACCESS DOOR CUTOUT 520CB, 520DB, 520EB, 520GB, 520JB, 520LB, 520MB, AND 520QB. REPLACED RUB STRIPS.

Part: DIAPHRAGM — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACK ON DIAPHRAGM AT STA 200 X=12. REPAIRED IAW SRM 51-11-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACKED FRAME CLIP AT STA 1486 BETWEEN LONGERONS 1-2 AT AFT ACCESSORY COMPARTMENT. REPLACED IAW DWG 9953016 AND SRM 51-30-05.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACKED FRAME CLIPS STA 1508 BETWEEN LONGERONS 3L - 3R AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-30-05 AND DWG 9911860.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

FUSELAGE SKIN DOUBLER AT L1 DOOR GUST LOCK HOUSING WORN. REPLACED IAW SRM 53-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

EXCESSIVE CORROSION ON LEFT HAND CUSP WEB, STA 460-470, X=54 - 60. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02 AND 51-30-05.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACKED L1 DOOR BEAM NR 6. REPAIRED IAW ERA 498178-14MA, REV O.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FLOOR SUPPORT RIGHT HAND SIDE STA 200 BETWEEN X=-7 TO X=-54. REPLACED FLOOR SUPPORT IAW SRM 53-10-014 AND 51-30-02.

Part: SKIN — CRACKED (L1 DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACKED L1 DOOR EXTERNAL SKIN AT HANDLE CUTOUT. REPAIRED IAW ERA 501106-14 MA, REV B.

Part: FLOOR SUPPORT — CORRODED (BS 210) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FLOOR SUPPORT, BS 210, RBL 11. REPLACED THE FLOOR SUPPORT IAW SRM 51-30-01.

Part: FLOOR SUPPORT — CORRODED (BS 148-200) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON FLOOR SUPPORT BS 148 TO 200, RBL 54. REPLACED IAW SRM 51-30-02.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 42,931 hrs · 28,332 cycles

WEAR ON FORWARD & AFT PRODUCTION DOUBLER OF CENTER CARGO DOOR. REPLACED IAW SRM 51-30-02.

Part: ATTACH FITTING — DELAMINATED (ANTI FLOAT TAB) · airframe 42,931 hrs · 28,332 cycles

DELAMINATION ON ANTI-FLOAT TAB AROUND ATTACH POINT, NR 3. REPAIRED IAW SRM 55-21-01.

Part: BEAM — CRACKED (R1 DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACK ON FORWARD ANGLE ON THE R1 DOOR BEAM NR 1. REPLACED IAW SRM 51-30-04, 51-30-05, AND DWG 9911579, REV L.

Part: PAN — CRACKED (BS 1098-1117) · airframe 42,931 hrs · 28,332 cycles

CRACK ON RIGHT UPPER RING PAN BETWEEN BS 1098 TO 1117. REPAIRED IAW SRM 56-20-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CORROSION ON LEFT HAND FLOOR SUPPORT, STA 148-200 X=7. REPLACED IAW SRM 51-30-01, 51-10-05 AND 51-10-03.

Part: PAN — CRACKED (CARGO DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACKED OUTER PAN UPPER EDGE OF CENTER CARGO DOOR, BS 731. REPAIRED IAW SRM 52-30-02.

Part: BEAM — CRACKED (L1 DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACKED L1 DOOR BEAM NR 7 AFT EDGE. REPAIRED IAW SRM 52-10-02. (LP# 0035821)

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 42,931 hrs · 28,332 cycles

EXCESSIVE CORROSION ON FLOOR SUPPORT BS 160-200, LBL 44. REPLACED IAW SRM 51-30-05 AND 51-30-02.

Part: SKIN — CRACKED (NLG DOOR FRAME) · airframe 42,931 hrs · 28,332 cycles

CRACKS ON FUSELAGE SKIN ON RIGHT AFT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED IAW SRM 53-30-01.

Part: CUSP WEB — CRACKED (BS 208-208) · airframe 42,931 hrs · 28,332 cycles

CRACKED CUSP WEB MEMBRANE, BS 205-208, BETWEEN LBL 54 TO 60. REPAIRED IAW SRM 51-11-01.

Part: SEAT TRACK — CORRODED (BS 1156-1160) · airframe 42,931 hrs · 28,332 cycles

CORRODED SEAT TRACK, BS 1156 - 1160, LBL 44. REPAIRED IAW SRM 53-40-01.

Part: PAN — CRACKED (BS 427) · airframe 42,931 hrs · 28,332 cycles

CRACK ON PAN UNDER FITTING NR 3, BS 427 FORWARD CARGO DOOR. REPAIRED IAW SRM 52-30-02.

Part: BEAM — CRACKED (PAX DOOR) · airframe 42,931 hrs · 28,332 cycles

CRACKED NR 1 DOOR BEAM ON THE FORWARD & AFT EDGE. REPAIRED THE BEAM IAW SRM 52-10-02.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 42,931 hrs · 28,332 cycles

CRACKED INNER DOUBLE AT AFT CONDITIONED AIR GROUND CONNECTION PANEL. REPLACED.

Part: SKIN — DENTED (L1 DOOR) · airframe 42,473 hrs · 28,097 cycles

SMALL DENT FOUND ON LOWER FORWARD EDGE OF L1 DOOR SKIN AFT OF LOWER FORWARD CORNER. REPAIRED IAW SRM 52-01-01.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 42,466 hrs · 28,091 cycles

TWO EMERGENCY CEILING LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REWIRED CENTER LIGHT ASSEMBLY AND SECURED A LOOSE CONNECTOR. OPS CHECKED GOOD.

Part: LANYARD — BROKEN (GIRT BAR) · airframe 42,258 hrs · 27,987 cycles

R1 GIRT BAR LANYARD BROKEN. REPLACED LANYARD ASSEMBLY.

Part: CAM — CONTAMINATED (AILERON) · airframe 41,927 hrs · 27,814 cycles

AILERONS BINDING DURING FLIGHT CONTROL CHECK. FOUND SAND AND DEBRIS STUCK TO CAM FOLLOWER PLAT ON TOP OF MIXER. CLEANED. OPERATION CHECKS GOOD. (LP# 9461644)

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,105 hrs · 27,288 cycles

FORWARD PASSENGER DOOR HOLD OPEN BAR AREA SKIN IS CRACKED AND DAMAGED. REPAIRED IAW SRM 53-30-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,105 hrs · 27,288 cycles

LEFT WHEEL WELL DOOR CUT OUT CRACKED. REMOVED AND REPLACED CHANNEL AND ANGEL IAW DWG 5930584. (LP# 2679140)

Part: PIN — OUT OF POSITION (EVAC SLIDE) · airframe 40,581 hrs · 26,987 cycles

FOUND L1 DOOR SLIDE RETAINING PIN OUT. R & R SLIDE.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 40,289 hrs · 26,819 cycles

HYDRAULIC FLUID COMING OUT OF RAM AIR DOOR. APU CONTAMINATED WITH HYDRAULIC FLUID. CABIN SMELLS LIKE HYDRAULIC FLUID. APU SHUTDOWN. FOUND RT THRUST REVERSER ACCUMULATOR HYDRAULIC LINE B-NUT LOOSE. TIGHTENED SAME. LEAK CHECK OK. COMPLY WITH DUCT BURNOUT AND REPLACEMENT OF COALESCER BAGS.

Part: CONTROL VALVE — FAILED (LT A/C PACK) · airframe 39,023 hrs · 26,075 cycles

STRONG ELECTRICAL SMELL ON FINAL. SMOKE IN COCKPIT AND CABIN. FOUND LEFT ACM SEIZED. R & R ACM AND LT PACK TEMP CONTROL VALVE IAW AMM. OPERATION CHECKS OK. PERFORMED DUCT BURNOUT IAW MM. NO ODOR NOTED.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 37,603 hrs · 25,220 cycles

LT HORIZONTAL STABILIZER HAS A CRACK INDICATION ON UPPER SURFACE OF AFT SKIN PANEL NEAR BARREL NUT HOLE. COMPLIED WITH PRI 536367-14AD, ERA 536367-14AD, REV O.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 37,620 hrs · 25,231 cycles

CRACK ON LT HORIZONTAL STABILIZER. REPAIRED IAW ERA 536367-14 AD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,088 hrs · 24,226 cycles

EMERGENCY LIGHTS ON SEATS ARE INOPERATIVE. R & R POWER SUPPLY AND BATTERIES. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 35,784 hrs · 24,014 cycles

OTBD SEAT TRACK BELOW G2 GALLEY CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DWG 5930547.

Part: ATTACH FITTING — CORRODED (LT MLG ACTUATOR) · airframe 35,784 hrs · 24,014 cycles

LT MLG ACTUATOR BUSHING BORE CORRODED. ACCOMPLISHED PRI 528692-14AD, REV ORIGINAL FINAL ERA 528692-14AD, REV ORIGINAL.

Part: SUPPORT FITTING — DAMAGED (MLG ACTUATOR) · airframe 35,784 hrs · 24,014 cycles

MLG ACTUATOR SUPPORT FITTING DAMAGED. REPAIRED IAW 5740-01140

Part: CABLE — MISROUTED (GIRT BAR) · airframe 35,451 hrs · 23,815 cycles

L1 DOOR DID NOT ARM PROPERLY. FOUND GIRT BAR CABLE MISROUTED. REPOSITIONED CABLE. OK FOR CONTINUED SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 34,357 hrs · 23,129 cycles

DIVERTED DURING CLIMBOUT PASSING THROUGH 12000 FT, F/A HEARD AFT LAVATORY SMOKE DETECTOR CHIRP AND SMELLED ELECTRICAL SMOKE. COULD NOT DETERMINE SOURCE AND NO OTHER INDICATIONS. INSPECTED ALL WIRING AND SWITCHES, NTF. ALL LIGHTS GOOD. CYCLED DIMMER SWITCHES SEVERAL TIMES, NTF. INSPECTED APU INLET FOUND CLEAN. SMOKE DETECTORS OPS CHECK GOOD. PERFORMED DUCT BURNOUT IAW FIM 21-22. NO ODOR NOTICED.

Part: MOUNT — DAMAGED (RADAR ALTIMETER) · airframe 33,906 hrs · 22,822 cycles

DURING WALKAROUND, FOUND EVIDENCE OF CORROSION, RADAR ALTIMETER ANTENNA HAD PULLED RIVETS. MAINTENANCE R & R MOUNTING PLATES.

Part: CABLE — OUT OF RIG (TAIL) · airframe 30,759 hrs · 21,057 cycles

DURING INSPECTION AND RIG CHECK OF CATWALK, MX RIGGED CABLES. OPS CHECKS GOOD. ACFT OK FOR SERVICE.

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 30,548 hrs · 20,922 cycles

ON DESCENT, ABOVE 18000, FLIGHT ATTENDANT REPORTED STRONG BURNING ODOR AND SMOKE COMING FROM VENTS, SPECIFICALLY IN BACK OF CABIN. CREW REPORTED INCREASING PACK CABIN TEMPERATURE SEEMED TO DECREASE ODOR. MAINTENANCE TROUBLESHOT PER FIM. FOUND COALESCER BAGS VERY DIRTY. PERFORMED DUCT BURNOUT PER AMM. REPLACED COALESCER BAGS. ALL CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,139 hrs · 20,135 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND RIGHT CEILING EMERGENCY LIGHT INOPERATIVE, ROW 38DEF. MAINTENANCE REMOVED AND REPLACED AFT POWER SUPPLY, ABOVE FLIGHT ATTENDANT STATION. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,316 hrs · 19,751 cycles

RAMP REPORTS DENT AFT OF C-3 BIN DOOR. MAINTENANCE FOUND DENT 5 FEET AFT OF C-3 CUTOUT, 39 INCHES BELOW CUSP/SPLICE (FLOOR LINE). DENT IS 9 INCHES LONG, 1 INCH WIDE AND .25 INCHES DEEP. REFERENCE SRM 53-30-02 TABLE 3 CONDITION 2. ACCOMPLISH REPAIR WITHIN 500 FLIGHT HOURS. DATA RETRIEVAL COMPLIED WITH.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 27,965 hrs · 19,565 cycles

FLIGHT CREW REPORTED ELECTRICAL SMELL IN FORWARD GALLEY. TURNED OFF GALLEY POWER AND SMELL DISSIPATED. MAINTENANCE REPLACED FORWARD GALLEY OVERHEAD LIGHT BALLAST. OPERATION CHECKS GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 27,946 hrs · 19,558 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY PHOTOLUMINESCENT LIGHT STRIPS MISSING THROUGHOUT CABIN. MAINTENANCE REPLACED PHOTO LUMINESCENT EMERGENCY PATHWAY LIGHT STRIPS PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT IS OKAY FOR SERVICE.

Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

AFT FUSELAGE LT VERTICAL STABILIZER ATTACH ANGLE STA 1520.225 REPAIR IAW ERA 489839-14, C/W ERA 489839-14.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 27,544 hrs · 19,331 cycles

HMV2 CABIN SEAT TRACK AT FS 495 BS 11 CRACKED. REPAIRED SECTION OF TRACK BETWEEN STA 495-531 PER MD90 SRM 53-40-01 VOL 1.

Part: BEAM — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

FUSELAGE AFT CARGO LOWER DOOR SURROUND STRUCTURE BEAM L-29R CORROSION REPAIR IAW ERA 489835-14. C/W ERA 489835-14.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,544 hrs · 19,331 cycles

HMV2 MID CARGO STA 826-845 LT FLOOR TRACK CORRODED. REPLACED TRACK SECTION PER MD90 SRM 53-10-01 AND DRWG 5936594.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

FORWARD FUSELAGE E & E DOOR CUTOUT INTERNAL DOUBLER CORROSION DAMAGE WAS REPAIR IAW 489840-14. C/W 489840-14.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,544 hrs · 19,331 cycles

HMV2 MID CARGO STA 674-769 L29L FLOOR SUPPORT CORRODED. REMOVED AND REPLACED TRACK PER MD90 SRM 53-10-01 AND DRWG 5965421.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 MID CARGO STA 598-693 RT FLOOR SUPPORT CORRODED. REPAIR PER MD90 SRM 53-40-01 VOL 1 PG 42 AND 43.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 MID CARGO STA 541 LT FLOOR SUPPORT CORRODED. REPAIR PER MD90 SRM 53-40-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 FWD CARGO STA 503 LT SUPPORT CORRODED. REPAIR PER MD90 SRM 53-40-01 VOL 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 FWD CARGO STA 522 RT FLOOR SUPPORT CORRODED. REPAIR PER MD90 SRM 53-00-01.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 27,544 hrs · 19,331 cycles

HMV2 STA 218-237 SIDEWALL SUPPORT CORRODED. REPAIR PER MD90 SRM 53-40-01 VOL 1 FIG 7.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 STA 1443 AFT SIDE OF FRAME HAS CORROSION FROM L30-L27R. REPLACED CHORD PER MD90 SRM 51-30-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 FWD E/E BAY CORROSION ON INTERNAL DOUBLER STA 140-160 L28L-L28R. REPAIR PER ERA 489840-14 REV ORIG.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 CORROSION AT FS 826-864 L29R. REPAIRED PER ERA 490979-14 REV ORIG.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 TAIL COMP STA 1437 LT FRAME AT 10 0 CLOCK POS FWD WEB DAMAGED. REPAIR PER MD90 SRM 51-11-01 FIG 2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 PAX CABIN RT CUSP WEB CORRODED STA 370. REPAIR PER MD90 SRM 53-20-02 VOL 1 AND SG DRWG 09530019.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 MID CARGO STA 704 WEB UPPER DOOR CUTOUT CORRODED. REPAIR PER ERA 490973-14 REV ORIG.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 AFT PRESSURE BULKHEAD CORRODED BL 0 STA 1395 LOWER. INSTALLED NEW DOUBLER PER MD90 SRM 51030-05 VOL 2 AND DRWG 5910130.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 AFT AIR STAIR COMPARTMENT FRAME 1542.019 CRACKED. REPAIR PER MD90 SRM 53-10-02 PG 72 VOL 1.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 27,544 hrs · 19,331 cycles

HMV2 CENTER WING BOX FS 883 RT STIFFENER CRACKED. REPAIRED PER ERA 489826-14 REV ORIG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,544 hrs · 19,331 cycles

HMV2 AFT CARGO FS 1053-1204 RT CARGO TRACK CORRODED. REPLACED CARGO TRACK PER MD90 SRM 51-00-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,544 hrs · 19,331 cycles

HMV2 AFT CARGO FS 1053 TO FS 1204 RT CARGO TRACK CORRODED. REPLACED CARGO TRACK PER MD90 SRM 51-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 AFT CARGO FS 1136 FLOOR SUPPORT CORRODED. REPLACED SUPPORT PER MD90 SRM 51-30-02 PG 1 VOL 2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,544 hrs · 19,331 cycles

HMV2 AFT CARGO FS 1053-1307 LT CARGO TRACK CORRODED. SPLICED IN NEW SECTION PER MD90 SRM 53-40-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 MID CARGO STA 598 CENTER FLOOR SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED PER ERA 490976-14 REV A.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 27,544 hrs · 19,331 cycles

HMV2 MID CARGO STA 769-845 RT FLOOR PANEL ATTACH ANGLE CORRODED. REPLACED TRACK PER MD90 SRM 51-00-00.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 27,544 hrs · 19,331 cycles

HMV2 CENTER WING BOX STA 883 LT STIFFENER CRACKED. REPAIRED PER ERA 489826-14 REV ORIG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 19,468 hrs · 13,664 cycles

PERFORMED TASK CARD 65034156 CORROSION ON RIGHT TRACK STA 522 & 788 MID CARGO COMPARTMENT SRM 53-30-01 VOL FIG 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,468 hrs · 13,464 cycles

PERFORMED TASK CARD 65033987 CORROSION ON SEAT TRACK BETWEEN STA 1184 & 1288 OF AFT CABIN SRM 53-40-01 VOL 1 FIG 6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,468 hrs · 13,464 cycles

PERFORMED TASK CARD 65034006 CORROSION ON SEAT TRACK BETWEEN STA 1260 & 1290 OF AFT CABIN SRM 53-40-01 VOL 1 FIG 6.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 19,468 hrs · 13,464 cycles

PERFORMED TASK CARD 65034007 CRACK ON L/E OF RIGHT MAIN LANDING GEAR FWD DOOR JAMB SRM 53-60-02 VOL 1 FIG 6. JAMB REPLACED THIS HMV.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,468 hrs · 13,464 cycles

PERFORMED TASK CARD 65033952 CORROSION ON R2 TRACK AT STA 240 OF CABIN SRM 53-40-01 VOL 1 FIG 6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,468 hrs · 13,464 cycles

PERFORMED TASK CARD 65033951 CORROSION ON R1 TRACK AT STA 240 OF CABIN SRM 53-40-01 VOL 1 FIG 6.