N14816

Part: LIGHT — INOPERATIVE (CABIN)

A/C IN SYR, PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

A/C IN SYR. PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHTS INOPERATIVE AT ROW 26. REMOVED AND REPLACED POWER SUPPLY IAW MM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW MM.

Part: BATTERY — WEAK (EMERGENCY LIGHT) · airframe 58,087 hrs · 27,667 cycles

AIRCRAFT IN MAINTENANCE, SYR, 4 INTERIOR EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED BATTERIES IN 4 SEPARATE POWER SUPPLIES IAW MM.

Part: PROXIMITY SWITCH — STICKING (TAIL CONE) · airframe 57,926 hrs · 27,591 cycles

IB FLIGHT, APPROXIMATELY 10 MINUTES BEFORE LANDING, TAIL CONE ANNUNCIATOR ILLUMINATED AND REMAINED ON. QRH PROCEDURE FOLLOWED. NO EMERGENCY DECLARED. UNEVENTFUL LANDING. FOUND DOOR PROXIMITY SWITCH STICKING. CLEANED AND LUBRICATED SWITCH.NO OTHER DEFECTS NOTED. OK FOR CONTINUED SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

IN INSPECTION, VARIOUS EMERGENCY EXIT LIGHTS OUT OVERHEAD. REMOVED AND REPLACED 3 BATTERY CHARGERS SERIAL NUMBERS 5227 15955 21872 AND AND 4 EMERGENCY BATTERIES PART NUMBER 5014.

Part: SLIDE — OUT OF POSITION (L1 DOOR)

AT GATE IN CZM, THE L1 DOOR SLIDE FELL OUT OF ITS COVER. REINSTALLED L1 DOOR SLIDE COVER.

Part: COMPRESSOR — FAILED (NR 1 ENGINE) · airframe 56,606 hrs · 26,958 cycles

THE AIRFRAME SHUDDERED SLIGHTLY AND WAS ACCOMPANIED BY AN AUDIBLE BOOM AFTER TAKEOFF FROM IAH AT ABOUT 3,000 FEET. THE NR 1 ENGINE SUBSEQUENTLY AUTO SHUTDOWN. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. INITIAL FINDINGS REVEALED METAL IN THE TAILPIPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. EXAMINATION OF THE ENGINE REVEALED HEAVY DAMAGE TO THE HPC 12TH AND 13TH STAGES WITH METAL IN THE TAILPIPE FROM HPC STATOR VANE. THE ENGINE WAS NEVER REPAIRED. THE AIRCRAFT IS EXITING THE CONTINENTAL FLEET.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,282 hrs · 26,801 cycles

INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 1418, L2L TO L2R. REMOVED AND REPLACED BELTFRAME IAW SRM 51-30-05.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 51,464 hrs · 24,300 cycles

EMERGENCY LIGHTS AT REAR GALLEY DOOR AND TAIL CONE DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY VASE PER MM 33-53-00 PG 407.

Part: SKIN — DENTED (CARGO DOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED AT CENTER OF DOOR 15 INCHES FROM FORWARD EDGE. THE DENTED AREA WAS REMOVED AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 2 AND 51-10-3.

Part: DOUBLER — DAMAGED (LT ELEVATOR TIP) · airframe 50,273 hrs · 23,622 cycles

INSPECTION FOUND LT ELEVATOR TIP TRAILING EDGE DOUBLER DAMAGED. THE DOUBLER WAS REPLACED IAW SRM 51-10-2 AND 51-30-8.

Part: DOUBLER — DAMAGED (LT ELEVATOR TIP) · airframe 50,273 hrs · 23,622 cycles

INSPECTION FOUND LT ELEVATOR TIP TRAILING EDGE DOUBLER DAMAGED. THE DOUBLER WAS REPLACED IAW SRM 51-10-2 AND 51-30-8.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED TWENTY INCHES BELOW LEFT PITOT PROBE AT FS 69.5. THE DENT WAS WORKED OUT TO ORIGINAL CONTOUR WITH NO CRACKS NOTED PER HFEC IAW MM 20-30-00. A PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 53-04, FIGURE 38.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AFT CARGO DOOR INNER SKIN CORRODED AROUND RIVET NUTS. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 52-05, FIGURE 7.

Part: CASTING — CRACKED (LT WING TIP) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LT WING TIP LEADING EDGE CASTING CRACKED WITH POPPED RIVETS AND GOUGES. THE CASTING PANEL WAS REMOVED AND A NEW CASTING PANEL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AFT PIT LT CARGO TRACK CORRODED. THE CARGO TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-3, 51-30-1, AND 51-30-5.

Part: FLOOR SUPPORT — BROKEN (CARGO BAY) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FORWARD CARGO COMPARTMENT LT FLOORBEAM SUPPORT BROKEN AT FS 294. THE FLOORBEAM SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-4.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AFT CARGO PIT LT VERTICAL SUPPORT TO FLOOR TRANSITION PANEL CORRODED AT STA 1155 - 1212. THE VERTICAL SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3 AND 53-01, FIGURE 1.

Part: ANGLE — CRACKED (CARGO DOORWAY) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AN 8 INCH CRACK IN FORWARD CARGO DOOR SEAL FLANGE OPEN LOCK ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FORWARD CARGO COMPARTMENT RT CARGO TIE DOWN TRACK CORRODED AT STA 218 - 370. THE TIE DOWN TRACK WAS REMOVED AND A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND CUSP WEB DOUBLER CORRODED AT STA 207-218, L18L. A NEW DOUBLER WAS INSTALLED IAW SRM 53-01-1, 51-10-3, AND 51-30-5.

Part: FITTING — DENTED (NR 5 SLAT) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LT WING NR 5 SLAT END FITTING DENTED. THE SLAT END FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4 AND 51-10-3.

Part: STRAP — CORRODED (TORQUE BOX) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR JAMB FORWARD TORQUE BOX LINER RETAINING STRAP CORRODED AND WORN AT STA 370. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-1 AND 51-10-3.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT STA 522 - 786. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN APB VERTICAL STIFFENER AT BL 0 ABOVE AFT ENTRANCE DOOR AT UPPER CORNER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, 51-30-5, 51-20-0, AND 51-30-2.

Part: SKIN — CORRODED (MID CARGO DOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND MID CARGO DOOR INNER SKIN CORRODED AROUND RIVET NUTS. THE RIVET NUTS WERE REMOVED. A DOUBLER AND RIVET NUTS WERE INSTALLED IAW SRM 51-30-1, 52-01, FIGURE 2, AND 51-30-2.

Part: DOUBLER — BENT (NLG DOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LEFT AFT NLG DOOR DOUBLER BENT AND SEPARATED AT AFT LOWER SECTION. THE DAMAGED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND A 1.5 INCH CRACK AND BEND IN LT HORIZONTAL STABILIZER TIP O/B LOWER AFT CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-11-0, 51-30-2, AND 51-30-3.

Part: FRAME — CRACKED (VENTRAL STAIRS) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND A 3 INCH CRACK IN FRAME FOR LEFT VENTRAL STAIRS SIDEWALL PANEL. THE SIDEWALL SUPPORT WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-1, 51-30-2, AND 53-01. REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-2. INSTALLED SIDEWALL SUPPORT IAW SRM 51-30-1.

Part: SKIN — GOUGED (RT TE FLAP) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND RIGHT WING FLAP T/E PANEL 1613 SKIN GOUGED AND PITTED. THE SKIN SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 57-50-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, RBL 12 - RBL 42. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: FITTING — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND RT FRAME TO FLOOR FITTING CORRODED AT STA 579, LONGERON 18R. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-3, 51-30-5, AND 51-30-1.

Part: SKIN — GOUGED (MLG DOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND RT MLG FORWARD DOOR SKIN GOUGED AT FORWARD UPPER CORNER. THE GOUGED AREA WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 52-01, FIGURE 1, 52-84-0, AND 51-10-3.

Part: STOP — CHAFED (MID CARGO DOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND MID CARGO DOOR STOP NR 12 CHAFED. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819.

Part: STRUCTURE — CORRODED (CABIN FLOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND SUB FLOOR WEB CORRODED AT STA 165 - 200, LBL 52. THE SUB FLOOR WAS REMOVED AND A NEW SUB FLOOR WAS INSTALLED IAW SRM 53-01, FIGURE 1, 53-05, FIGURE 1, 51-10-3, 51-30-5, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, RBL 9 - RBL 45 AND AT LBL 5 - RBL 5. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-10-3.

Part: SKIN — GOUGED (NLG DOOR) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LT FORWARD NLG DOOR SKIN GOUGED AT FORWARD UPPER CORNER. THE GOUGED AREA WAS REMOVED IAW SRM 52-01, FIGURE 1. REPAIR PARTS WERE INSTALLED IAW SRM 52-01, 52-84-0, 51-10-3, AND 51-30-2.

Part: CHANNEL — TORN (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AFT EMERGENCY EXIT RAMP UPPER LEFT RAIL CHANNEL EDGE TORN AT FS 1474 WITH A LARGE DENT 20 INCHES AFT. THE TORN EDGE WAS BLENDED OUT AND REPAIR DOUBLERS AND ANGLES WERE INSTALLED IAW SRM 53-01, FIGURE 1 & 2, 51-10-4, 51-10-3, AND 51-30-2. THE DENT WAS REFORMED IAW SRM 51-10-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED AT STA 216, RBL 55. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, 51-30-5.

Part: STOP — CHAFED (CARGO DOORWAY) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND MID CARGO DOOR STOPS NR 3, 4, 6 & 8 CHAFED. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5330-02819.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1185, LONGERON 18L. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5331-2-A0800.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 160 - 200, RBL 44 AND AT STA 148 - 200, RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED ON LOWER SURFACE AT STA 218 - 256, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4.

Part: RIB — GOUGED (NR 15 SLAT TRACK) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LEFT WING O/B EDGE OF RIB GOUGED AT NR 15 SLAT TRACK CUTOUT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-30-2, 51-30-6, 51-30-4, 51-10-3, AND 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND TWO, 1 INCH CRACKS IN E&E COMPARTMENT CABIN PRESSURE WEB AT STA 190, RBL 48. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, 51-30-3, AND 51-30-2.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORT ANGLE AND PLATE CORRODED AT FS 148 - 200, RBL 55. THE ANGLE AND PLATE WERE REMOVED AND A NEW ANGLE AND PLATE WERE INSTALLED IAW SRM 51-30-2 AND 51-10-4.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FORWARD CABIN LT CUSP WEB AT STA 168 - 237, LONGERON 18L. REPAIRED IAW EA 9-5310-2-A0798 AND ECRA 5310-04076.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND EPC PANEL SUPPORT ANGLE AT FLOOR LINE CORRODED AT STA 160, LBL 12 - LBL 44. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: SKIN — GOUGED (TE FLAP) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND RT WING NR 4 FLAP O/B TRAILING EDGE SKIN GOUGED. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 200 - 266, RBL 22. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-01, FIGURE 4F, 51-10-3, AND 53-05, FIGURE 4F.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AN 18 INCH CRACK IN FLOORBOARD WEB AT STA 1022, LBL 50. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-01, FIGURE 4 AND 53-01, FIGURE 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LT EXTERIOR FUSELAGE SKIN CREASED AT STA 218 FROM LONGERON 16L - 18L. THE SKIN WAS REFORMED TO ORIGINAL CONTOUR IAW SRM 53-04, FIGURE 38, TABLE C. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, VIEW G, AND 51-10-3.

Part: WEB — CRACKED (TORQUE BOX) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR TORQUE BOX WEB, APPROXIMATELY LONGERON 15L. A DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5314-2-A0799, SRM 51-10-4, AND 51-10-3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND GALLEY SUPPORT FITTINGS CORRODED AT STA 160, RBL 45 AND RBL 50. THE SUPPORT FITTINGS WERE REMOVED AND NEW FITTINGS WERE INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3.

Part: PANEL — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND MID PIT RT BULKHEAD PANEL METAL FRAME CORRODED AT FS 788. THE CORROSION WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-10-3, 53-24-01, 53-01, FIGURE 2, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, LBL 12 - LBL 38. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1031 - 1089. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-5, 51-30-1, 51-10-4, 51-30-2, AND 51-10-3.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AROUND FASTENER HOLES AT STA 965, BL 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-3 AND 51-30-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 200 - 265. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, 51-30-2, 51-30-5, 51-30-1, 51-10-4, AND 51-10-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LT EXTERIOR FUSELAGE SKIN DENTED AT STA 229 - 276 BETWEEN LONGERONS 15L AND 19L. THE DENTED SKIN SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160 - 197, LBL 44. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-01, FIGURE 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND AFT PIT UPPER FLOOR SUPPORT TOP RAIL CORRODED AT EACH CLIP NUT HOLE, FS 1309 BETWEEN LAV WALLS. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-3, 51-10-3, AND 51-30-5.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND MID CARGO RIGHT TIE DOWN TRACK CORRODED AT STA 693 - 786. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-3, 51-10-4, AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND MID CARGO FLOOR SUPPORT CORRODED ON INNER AND OUTER SURFACES AT FS 786 BETWEEN LONGERONS 28R AND 27R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND WEB CORRODED AT STA 200 - 216, RBL 55 AFTER REMOVAL OF GALLEY SUPPORT FITTING. THE CORRODED AREA WAS CUT OUT AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 53-01, FIGURE 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 160 - 196, LBL 54. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-2, 53-01, FIGURE 1, 51-10-3, AND 51-30-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LT EXTERIOR FUSELAGE SKIN DENTED AT STA 266, LONGERON 22L. RIVETS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2, 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,271 hrs · 23,621 cycles

INSPECTION FOUND LT EXTERIOR FUSELAGE SKIN DENTED AT STA 302, LONGERON 23L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2.

Part: POWER SUPPLY — INOP (EMER EXIT)

FORWARD OVERWING EMERGENCY EXIT LIGHT STAYS ON CONTINUOUSLY. REPLACED POWER SUPPLY PER MM 33-53-00.

Part: ACTUATOR — INOPERATIVE (LT MLG)

THE LEFT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED WITH THE YELLOW GEAR DOOR LIGHT ON AFTER GEAR RETRACTION LEAVING IAH. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG RETRACT CYLINDER PER MM 32-32-02. A GEAR SWING WAS PERFORMED AND ALL OPERATION AND INDICATIONS CHECKED GOOD.

Part: FRAME — CRACKED (BS 1418)

BELT FRAME CRACKED AT STATION 1418 LONG 2 LT AND RT 1. REPAIRED BELT FRAME PER SRM 53-03-32.

Part: STATOR SUPPT — BROKEN (NR 2 ENGINE)

THE NR 2 ENGINE BEGAN TO VIBRATE ACCOMPANIED BY AN ERRATIC EPR GAGE READING WHILE EN ROUTE. ENGINE POWER WAS REDUCED TO IDLE, ATTEMPTS TO OBTAIN MORE THAN 50 PERCENT POWER CAUSED EXCESSIVE VIBRATION. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. A BORESCOPE INSPECTION FOUND DAMAGE TO THE NR 2 ENGINE. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REVEALED AN 8TH STAGE STATOR SUPPORT(SHELF) BROKEN.

Part: STATOR VANE — FAILED (NR 1 ENGINE)

THE NR 1 ENGINE COMPRESSOR STALLED AT 37,000 FEET WHEN POWER WAS REDUCED FOR DESCENT. THE STALL WAS ACCOMPANIED BY TWO BANGS AND SUBSEQUENT YAW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP TEARDOWN FINDINGS REVEALED FAILURE OF A C-7 STATOR VANE.

Part: ACTUATOR — LEAKING (LT MLG)

FLT NR 1078 - IAH - THE RIGHT HYDRAULIC QUANTITY DROPPED WITH PRESSURE DROPPING TO ZERO WHILE EN ROUTE FROM COS TO IAH. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG RETRACT ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-02 AND LEAK CHECK WAS GOOD. (M)

Part: O-RING — LEAKING (RT MLG WW)

FLT NR 0208 - MCO - THE RIGHT HYDRAULIC SYSTEM SHOWED A DECREASE IN QUANTITY FROM 17 QUARTS TO 3 QUARTS WHILE EN ROUTE FROM IAH TO MCO. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE O-RING AT FITTING ON BRAKE CONTROL VALVE IN RT WHEEL WELL LEAKING. THE O-RING WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. (M)