N14839

Part: BATTERY PACK — INOPERATIVE (STA 1338R) · airframe 46,601 hrs · 22,784 cycles

THE TAILCONE SLIDE EMERGENCY LIGHTS WOULD NOT TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.

Part: LATCH — OUT OF RIG (TAILCONE) · airframe 45,528 hrs · 22,211 cycles

THE TAILCONE INTERIOR RELEASE HANDLE PULL WAS EXCESSIVE. THE TAILCONE LATCH LOCKPINS WERE ADJUSTED AND OPERATION CHECKED GOOD IAW MM 53-53-00.

Part: LONGERON — CRACKED (STA 1418) · airframe 45,528 hrs · 22,211 cycles

INSPECTION FOUND A 1/4" CRACK IN LONGERON 2L AT BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18.

Part: CARGO TRACK — CORRODED (BS 1003 - 1155)

INSPECTION FOUND AFT CARGO RT TIEDOWN TRACK CORRODED AT FS 1003-1155. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-03, 51-30-01, AND 51-30-02.

Part: PANEL — CRACKED (RT WING ROOT)

INSPECTION FOUND A 3 INCH CRACK IN RT WING TRANSVERSE PANEL. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: CARGO TRACK — CORRODED (BS 636 - 1212)

INSPECTION FOUND MID AND AFT CARGO LT TIE DOWN TRACKS CORRODED AT FS 636-736 AND FS 1003-1212, LBL 24. THE CORRODED SECTIONS OF TRACK WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-1, AND 51-30-5.

Part: WEB — CORRODED (BS 1136 - 1212)

INSPECTION FOUND CABIN FLOOR WEB CORRODED AT SUPPORTS BETWEEN FS 1136 AND 1212. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1.

Part: DOOR PAN — GOUGED (CARGO DOOR)

INSPECTION FOUND AFT CARGO DOOR AFT STOP POSITIONS ON FRAME GOUGED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND ECRA5230-01519.

Part: FLOORBEAM — CORRODED (BS 1155)

INSPECTION FOUND AFT CARGO FLOOR PANEL SUPPORT CORRODED AT FS 1155, LBL 16 TO RBL 8. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.

Part: STOP PAD — CHAFED (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR FORWARD STOP PADS ON FRAME CHAFED. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-03, AND EA 9-5233-A0988.

Part: INTERCOSTAL — CRACKED (BS 1022 - 1041)

INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT FS 1022-1041, BL 0. THE INTERCOSTAL WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: CARGO TRACK — CORRODED (BS 769 - 786)

INSPECTION FOUND RT CARGO TIEDOWN TRACK IN MID CARGO COMPARTMENT CORRODED AT STA 769-786. A NEW CARGO TIEDOWN TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-10-3.

Part: FITTING — CORRODED (BS 1140)

INSPECTION FOUND LEFT O/B GALLEY FITTING CORRODED AT FS 1140. THE GALLEY FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.

Part: BRACKET — CRACKED (RT WING)

INSPECTION FOUND RT FORWARD ADF FAIRING SUPPORT BRACKET CRACKED AT L/E WING ROOT. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Part: INTERCOSTAL — GOUGED (BS 1007)

INSPECTION FOUND AFT CARGO COMPARTMENT INTERCOSTAL GOUGED ON TOP AND BOTTOM FLANGE AT STA 1007, LONGERON 22R. REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-01, FIGURE 2.

Part: SKIN — CHAFED (CARGO DOOR)

INSPECTION FOUND LOWER EXTERNAL SKIN FORWARD AND AFT CORNERS OF FORWARD CARGO DOOR CHAFED. A TWO DOUBLER REPAIR WAS INSTALLED WITH SHIMS IAW SRM 52-05, FIGURE 4, PAGE 5 AND 51-30-2, FIGURE 4, PAGE 5.

Part: SKIN — DENTED (ELEVATOR)

INSPECTION FOUND LT ELEVATOR LOWER SKIN SURFACE DENTED. THE DENTED AREA WAS REMOVED AND REPAIRED IAW ECRA 5520-01231.

Part: STOP PAD — CHAFED (DOOR FRAME)

INSPECTION FOUND AFT CARGO DOOR UPPER STOP AND FORWARD STOP PADS ON FRAME CHAFED. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, 52-03, FIGURE 8, AND ECRA 5230-01519.

Part: FRAME — CHAFED (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR UPPER FORWARD STOP AREA CHAFED. A DOUBLER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 52-03, FIGURE 8 AND ECRA 5230-01518.

Part: SKIN — CORRODED (CARGO DOOR)

INSPECTION FOUND AFT CARGO DOOR UPPER FORWARD WEB SKIN CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-3. A DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-2.

Part: SKIN — CRACKED (BS 1485)

INSPECTION FOUND RT SIDE TAIL COMPARTMENT SKIN CRACKED JUST FORWARD OF RUDDER TRIM ACTUATOR AT STA 1485. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-14-4 AND 51-30-1.

Part: SKIN — DENTED (BS 636)

INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AT STA 636, LONGERON 30. THE SKIN WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 53-01, FIGURE 1, 51-30-05, AND 51-30-02.

Part: FLANGE — CHAFED (CARGO DOOR)

INSPECTION FOUND FORWARD PIT DOOR SEAL ATTACH FLANGE CHAFED UNDER STOP PADS AT ALL SIDES OF DOOR. REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, 51-30-7, 52-03, FIGURE 8 AND ECRA 5230-01518.

Part: CARGO TRACK — CORRODED (BS 1212 - 1322)

INSPECTION FOUND RT TIEDOWN TRACK IN AFT CARGO COMPARTMENT CORRODED AT STA 1212-1322, RBL 24. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4H AND 51-30-1.

Part: RIB — CRACKED (MLG DOOR)

INSPECTION FOUND A 1 INCH CRACK IN I/B TOP END OF FORWARD RIB ON LT MLG I/B DOOR. THE SKIN WAS REMOVED AND THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-05. THE SKIN WAS CLOSED IAW SRM 51-30-1, 51-30-2, AND 51-30-8.

Part: CLIP — CRACKED (VERTICAL STAB)

INSPECTION FOUND A 1 INCH CRACK IN CLIP AT VERTICAL STABILIZER LOWER LT AFT CORNER JUST FORWARD OF RUDDER LEADING EDGE. THE CLIP WAS REMOVED AND A NEW CLIP WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.

Part: SEAT TRACK — CORRODED (BS 1098 - 1231)

INSPECTION FOUND LT CENTER SEAT TRACK CORRODED FROM STA 1098 TO 1231. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 5.

Part: COWL — CRACKED (NR 2 ENGINE)

INSPECTION FOUND A 1 INCH CRACK IN INTERNAL DOUBLER STRAP OF NR 2 ENGINE NOSE COWL THROUGH ACCESS PANEL NR 7403 UPPER RT SIDE. THE NR 2 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-10-01.

Part: BEAM — CORRODED (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED AROUND RIVETS. A DOUBLER AND SPACER WERE INSTALLED IAW SRM 51-30-5 AND ECRA 5310-03027.

Part: SUPPORT — CORRODED (BS 168 - 200)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 168-200, RBL 47. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 53-14-1.

Part: SKIN — GOUGED (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR SKIN GOUGED. THE AREA WAS REPAIRED IAW SRM 52-05, FIGURE 1.

Part: SEAT TRACK — CORRODED (BS 218)

INSPECTION FOUND RT O/B SEAT TRACK CORRODED AT GALLEY FITTING FS 218. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F, 51-10-4, 51-10-3, 51-30-1, AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1140)

INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1140 GALLEY FITTING. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-05, 51-10-4, AND 51-30-1.

Part: DOOR PAN — CRACKED (CARGO DOOR)

INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO DOOR PAN AT T/E SEAL RETAINER HOLES FLANGE, LOWER FORWARD SECTION, 12 INCHES FROM BOTTOM. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 26A. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A, 51-10-4, 51-10-3, 51-30-2, AND 51-20-00.

Part: SEAT TRACK — CORRODED (BS 207)

INSPECTION FOUND RT INBD AND RT CENTER SEAT TRACKS CORRODED AT STA 207. THE SEAT TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, AND 53-05, FIGURE 4F.

Part: SKIN — CRACKED (MLG DOOR)

INSPECTION FOUND .5 INCH CRACKS IN REPAIR DOUBLER AT LOWER AFT O/B CORNER OF LT MLG I/B DOOR. THE CRACKED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 1079 - 1271)

INSPECTION FOUND LT I/B SEAT TRACK CORRODED FROM STA 1079-1271. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, 53-05, AND 51-30-2.

Part: DOOR PAN — CORRODED (CARGO DOOR)

INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED AROUND RIVETS. THE DOOR JAMB PAN WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 44.

Part: SEAT TRACK — CORRODED (BS 218)

INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 218. THE SEAT TRACK WAS REMOVED AND REPLACED USING A SPLICE IAW SRM 51-30-2,53-05, AND 51-30-3.

Part: PANEL — CORRODED (MLG DOOR)

INSPECTION FOUND FORWARD UPPER PANEL OF Rt MLG DOOR CORRODED. A NEW PANEL WAS INSTALLED IAW SRM 52-84-0.

Part: SEAT TRACK — CORRODED (BS 157 - 200)

INSPECTION FOUND SEAT TRACK CORRODED AT FS 157-200, LBL 14. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: SUPPORT — CORRODED (CABIN)

INSPECTION FOUND FLOOR SUPPORT AT FORWARD ENTRANCE THRESHOLD CORRODED. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1 AND 51-3-0.

Part: BRACKET — CORRODED (CABIN)

INSPECTION FOUND CORROSION AROUND FASTENER HOLE AT RT LOWER CORNER OF RT AFT EMERGENCY EXIT DOOR. THE CORROSION WAS REMOVED IAW SRM 51-10-3 AND 51-30-2. A BRACKET WAS INSTALLED IAW SRM 51-10-4 AND 51-30-1.

Part: SUPPORT — CORRODED (BS 180 - 200)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180-200, RBL 37. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-3, AND 51-30-5.

Part: SKIN — GOUGED (BS 484)

INSPECTION FOUND FUSELAGE SKIN GOUGED AT FS 484, L24R. THE GOUGED AREA WAS REMOVED IAW SRM 51-01, FIGURE 1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.

Part: SKIN — CREASED (BS 120 - 150)

INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 120-150 BETWEEN LONGERON 24 AND 25R. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 12B, 51-30-2, AND 51-30-5.

Part: FITTING — CORRODED (BS 200)

INSPECTION FOUND G-2 GALLEY FITTING CORRODED AT FS 200. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, AND 51-30-2.

Part: SUPPORT — CORRODED (STA 1153)

INSPECTION FOUND FLOOR SUPPORT BETWEEN CENTER AND INBOARD SEAT TRACKS AT STA 1153 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5, 53-14-3, FIGURE 12, AND 51-10-4.

Part: SKIN — CRACKED (BS 1345)

INSPECTION FOUND AFT ACCESSORY CATWALK SHROUD RT AND LT FWD END SKIN CRACKED AT FS 1345. THE CRACKS WERE 2 AND 1 LONG, RESPECTIVELY. THE CRACKS WERE STOP DRILLED AND REPAIRED IAW SRM 53-01, FIGURE 2.

Part: FITTING — CORRODED (BS 157)

INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED ATSTA 157, RBL 4. A NEW GALLEY SUPPORT FITTING WAS INSTALLED IAW SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 180)

INSPECTION FOUND FLOOR SUPPORT AT FORWARD ENTRY AREA, STA 180, LBL 25, CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-4, 51-30-5, AND 51-20-00.

Part: WEB — CRACKED (AIRSTAIR)

INSPECTION FOUND AFT AIRSTAIRS LEFT AND RIGHT LOWER WEB CRACKED ABOVE GROUND ROLLER. THE CRACKS WERE 2 AND 1 LONG RESPECTIVELY. REPAIR DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-01, FIGURE 1 AND 51-10-3 .

Part: SKIN — DENTED (BS 1291)

INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1291, L25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.

Part: LIGHT — INOPERATIVE (L1 DOOR)

A PREFLIGHT CHECK FOUND THE PORTABLE EMERGENCY LIGHT AT L-1 DOOR INOPERATIVE. THE PORTABLE EMERGENCY LIGHT WAS REMOVED AND REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE AFT CABIN EMERGENCY AISLE PATH LIGHTING BATTERY PACK HAD A LOW CHARGE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.

Part: ANGLE — CRACKED (DORSAL FIN)

INSPECTION FOUND DORSAL FIN ATTACH ANGLE ON RT SIDE CRACKED AT RIVET. A NEW ATTACH ANGLE WAS INSTALLED IAW EA 5340-01012.

Part: WEB — CORRODED (BS 1211)

INSPECTION FOUND CORROSION ON WEB UNDER TIEDOWN RAIL IN AFT BAGGAGE BIN AT STA 1211, RBL 13, NEAR LOWER AFT CORNER OF ENTRY. THE CORROSION WAS REMOVED. DOUBLER AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 53-01 AND 53-14-3.

Part: FRAME — CRACKED (BS 1418)

INSPECTION FOUND BELT FRAME CRACKED IN THREE PLACES AT STA 1418. THE CRACKS WERE LOCATED AT LONGERON 1, 2L, AND 2R AND MEASURED 1, .5 AND 2 INCH LONG RESPECTIVELY. THE FRAME WAS REPAIRED IAW ECRA 5310-03667.

Part: ANGLE — CORRODED (BAGGAGE COMPT)

INSPECTION FOUND CORROSION ON FLOOR SUPPORT ANGLE ATTACHED TO MID CARGO BIN AFT WALL, LOWER RT SIDE. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: WEB — CORRODED (CARGO COMPT)

INSPECTION FOUND FLOOR SUPPORT WEB ATTACHED TO MID CARGO AFT WALL CORRODED. THE WEB WAS REMOVED, AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS ON LEFT AND RIGHT SIDE INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-0.

Part: CABLES — OUT OF ADJUST (TAIL CONE)

THE PULL FROM EXTERIOR TAILCONE RELEASE HANDLE WAS LOW. THE TAILCONE CABLES WERE ADJUSTED.

Part: ANGLE — CORRODED (BS 1155-1211)

HOU - INSPECTION FOUND CORROSION IN Z-ANGLE ACROSS BOTTOM OF AFT BAGGAGE BIN DOOR OPENING AT STATION 1155 TO 1211. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. (M)

Part: DOOR PAN — CRACKED (AFT CARGO DOOR)

HOU - INSPECTION FOUND A 2 INCH CRACK UNDER FORWARD LATCH MECHANISM OF AFT CARGO DOOR PAN. A DOUBLER WAS INSTALLED IAW SRM 52-05. (M)

Part: SKIN — GOUGED (RT HORIZ STAB)

HOU - INSPECTION FOUND MINOR GOUGES ON RIGHT HORIZONTAL STABILIZER SKIN AT STATION XS 142. THE GOUGES WERE REMOVED BY BURNISHING OUT IAW SRM 55-01, FIGURE 1, PAGE 3. (M)

Part: ANGLE — BENT (PAX DOOR)

HOU - INSPECTION FOUND THE FORWARD LOWER EDGE OF MAIN CABIN DOOR OUTER SKIN BENT AND THE LOWER SUPPORT ANGLE WAS ALSO BENT. A NEW LOWER SUPPORT ANGLE WAS INSTALLED AND THE OUTER SKIN WAS STRAIGHTENED IAW SRM 52-01, FIGURE 1. (M)

Part: TE SKIN — CRACKED (RT TE FLAP)

HOU - INSPECTION FOUND A 7.5 INCH CRACK IN FIBERGLASS SECTION OF RIGHT WING INBOARD FLAP OUTBOARD TRAILING EDGE. A NEW SECTION OF TRAILING EDGE FLAP WAS INSTALLED IAW SRM 57-03, FIGURE 9. (M)

Part: SKIN — DENTED (BS 237)

HOU - INSPECTION FOUND A DENT IN SKIN WITH DAMAGE TO FORMER AT STATION 237 BETWEEN LONGERON 17L AND 16L. THE SKIN AND FORMER WERE REPLACED IAW EC 5330-02163. (M)

Part: ANGLE — CRACKED (BS 1463)

HOU - INSPECTION FOUND TWO .375 INCH CRACKS IN LEFT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE AT STATION 1463. THE CRACKED AREA WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 23. (M)

Part: BRACKET — CRACKED (BS 886)

HOU - INSPECTION FOUND A 1.125 INCH CRACK IN FUSELAGE BELLY PANEL 'T' BRACKET AT STATION 886 AIRCRAFT CENTERLINE. A NEW 'T' BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-3. (M)

Part: TEMP SENSORS — PLUGGED (CABIN)

GSO - FLT 0562 - BOTH THE RIGHT AND LEFT AIR CONDITIONING PACKS TRIPPED OFF WHILE AT FL 330. AN EMERGENCY DESCENT WAS PERFORMED AND OXYGEN MASKS DEPLOYED. ACFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CABIN TEMPERATURE SENSORS PLUGGED. SENSORS WERE CLEANED AND REINSTALLED. AIR CONDITIONING SYSTEMS TESTED AND PERFORMED PER MM 21-00-00, PAGES 503-506, AND RT SIDE WAS FOUND INOPERATIVE IN AUTO. CABIN TEMP WAS PLACARDED INOP IN AUTO PER MEL 21-29. IN ADDITION, MX FOUND ALL OXYGEN MASKS DEPLOYED. PASSENGER OXYGEN SYSTEM WAS PLACARDED INOPERATIVE PER MEL 35-02. CREW OXYGEN WAS VERIFIED FULL. (X)

Part: LINE — CRACKED (OIL PRESS)

FLT NR 0478 - GSO - THE NR 1 ENGINE BEGAN TO LOSE OIL WHILE EN ROUTE FROM TPA TO CLE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OIL LINE FROM THE OIL PRESSURE TRANSMITTER CRACKED. THE OIL LINE TO THE TRANSMITTER WAS REMOVED AND REPLACED. LEAKS CHECKS WERE GOOD. (M)

Part: SEALS — LEAKING (RT ACM)

FLT NR 0297 - IAH - A HOT OILY ODOR WAS OBSERVED IN THE CABIN WITH THE AIRFOIL ANTI-ICE ON, DURING TAKEOFF, APPROACH, AND LANDING PHASES OF FLIGHT. MAINTENANCE REPLACED THE PERI SEALS ON THE RT AIR CYCLE MACHINE OUT DUCT AND OPERATIONAL CHECKS WERE GOOD. (Z)