N950DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,134 hrs · 53,945 cycles

OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE ROWS 22-25. REPLACED THE BATTERIES.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 71,071 hrs · 53,094 cycles

EMERGENCY LIGHT AT 35D INOPERATIVE. FOUND HARNESS DAMAGED. REPLACED HARNESS IAW AMM 33-53. OPS NORMAL.

Part: CABLE — MISROUTED (TAILCONE) · airframe 69,937 hrs · 52,234 cycles

TAILCONE CABLE MISROUTED. NOT THROUGH TAILCONE FAIRLEAD. TAILCONE INSTALLED IAW AMD S5350-4642. CABLE ROUTED CORRECTLY.

Part: DOOR FRAME — CORRODED (BS 636-693) · corrosion level 2 · airframe 69,795 hrs · 52,138 cycles

MID CARGO LOWER DOOR FRAME HAS CORROSION BETWEEN BS 636 - 693. REPAIRED THE LOWER DOOR FRAME IAW PRI/ERA 553436-14.

Part: ANGLE — DAMAGED (AFT FUSELAGE) · airframe 69,795 hrs · 52,138 cycles

DENT AND CRACKED ANGLE AT AIRSTAIR CUTOUT 1 FT FWD OF AFT RT CORNER. REPAIRED IAW ER/A 553772-14.

Part: FRAME — DAMAGED (BS 1485) · airframe 69,795 hrs · 52,138 cycles

REPAIR ANGLE CRACKED AT LOWER END OF BS 1485 FRAME RT SIDE NEAR STAIR ACTUATING CYLINDER. REPAIRED IAW ER/A 553772-14.

Part: ACM — LEAKING (RIGHT) · airframe 69,795 hrs · 52,138 cycles

ON SHORT FINAL, SMELLED A SMOKE TYPE ODOR. FA STATED BOTH LAVATORY SMOKE DETECTORS ON CAPTAIN SIDE (FRONT & BACK) WENT OFF. A HAZE WAS OBSERVED IN THE CABIN. FOUND RIGHT ACM LEAKING OIL. REPLACED THE ACM. COMPLETED DUCT BURN-OUT.

Part: FITTING — CRACKED (RT WING) · airframe 69,795 hrs · 52,138 cycles

RT WING TE GROUND SPOILER ACTUATOR FWD FITTING CRACKED. REPLACED THE FITTING IAW DWG SR09570010 REV. H.

Part: BEAM — CORRODED (BS 636-693) · corrosion level 2 · airframe 69,795 hrs · 52,138 cycles

MID CARGO DOOR THRESHOLD BEAM SEVERAL AREAS OF CORROSION FROM BS 636 TO 693. REMOVED AND REPLACED THE BEAM IAW DWG 5936038.

Part: BUSHING — WORN (TAILCONE) · airframe 69,795 hrs · 52,138 cycles

TAILCONE RELEASE SYSTEM, T-PIN & BUSHING WORN FOR PULL CABLE. SEE NR FOR ADDITIONAL INFORMATION 031-0001:5350-01077-0101/002 00005 REPAIRED REF AMM 53-53-00.

Part: CLAMP — OUT OF ADJUST (TAILCONE) · airframe 69,795 hrs · 52,138 cycles

TAILCONE RELEASE SYSTEM, LOCKING CABLE CLAMP DOES NOT CLEAR LOWER END OF CONDUITS BY 1/2" REF AMDS CARD5350-01077-0101 STEP 7, D, 5. REPAIR REF AMM 53-53-00. OPS WILL BE PERFORMED ON AMDS 5350-01077-0101.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,795 hrs · 52,138 cycles

AFT CARGO DOOR THRESHOLD BEAM AND STRAP SEVERAL AREAS OF CORROSION FROM STA 1154 TO STA 1211 ALSO BETWEEN SKIN LAYERS NEAR AFT DOOR STOP. AFT CARGO THRESHOLD, BLENDED AFT BEAM LOWER SUPPORT FOUND WITHIN LIMITS PER SRM 53-01. REPLACED FWD BEAM LOWER SUPPORT ANGLE AND ALSO REPLACED THRESHOLD REPAIR STRAP (-9 SPACER) PER SRM 53-05 FIG. 123.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,795 hrs · 52,138 cycles

ERA 553436-14 SECTION 1 ISSUED FOR CORROSION DAMAGE TO C2 DOOR FRAME DOUBLER AND SKIN. ACCOMPLISH SECTION II INSPECTION EVERY 8000 CYCLES FOLLOWING SECTION I ER/A 88-553436.

Part: CABLE — FRAYED (TAILCONE) · airframe 69,795 hrs · 52,138 cycles

TAIL CONE KEVLAR CABLE FRAYING. A NEW KEVLAR CABLE WAS INSTALLED IAW AMM 53-53-00.

Part: CABLE — LOOSE (TAILCONE RELEASE) · airframe 69,795 hrs · 52,138 cycles

TAILCONE RELEASE SYSTEM, TEE PIN PULL CABLE HAS EXCESSIVE SLACK. REPAIRED IAW AMM 53-53-00. RIGGED THE CABLE IAW AMDS 5350-01077-0101.

Part: ENGINE — MAKING METAL · airframe 68,844 hrs · 51,400 cycles

RETURNED TO DEPARTURE, DUE TO AN OIL STRAINER CLOGGED MESSAGE. MAINTENANCE FOUND METAL ON THE MCD AND IN THE OIL FILTER. ENGINE CHANGE REQUIRED.

Part: DOOR — LACK OF LUBE (TAILCONE) · airframe 68,447 hrs · 51,098 cycles

DURING TAILCONE RELEASE FUCTIONAL CHECK FOUND ARMING HANDLE HARD TO ROTATE. LUBED DOOR IAW AMM 12-21. CONFIRMED RIGGING AND RELEASE FORCE IAW AMM 52-12. OPS CHECK GOOD.

Part: LINE — BROKEN (HYD SYSTEM) · airframe 67,847 hrs · 50,683 cycles

WHILE ENROUTE, THE FLIGHT DIVERTED TO MEM FOLLOWING THE "RT HYDRAULIC LOW" MESSAGE ILLUMINATING ALONG WITH THE RT HYDRAULIC QUANTITY RAPID DECREASING TO 2 QUARTS. COMPLETED CHECKLIST. NOTE: F/A REPORTED LOUD NOISE DURING CLIMBOUT BUT NO INDICATIONS OF ANY PROBLEMS UNTIL PASSING FL240. FOUND RT HYDRAULIC SYSTEM PRESSURE LINE FORWARD OF HYDRAULIC FILTER TO THE CHECK VALVE OF THE RUDDER SHUTOFF VALVE TO BE BROKEN. INSTALLED A TEMPORARY FLEXIBLE HOSE REPAIR IAW AMM 20-12-04. REINSPECTION REQUIRED W/I 175F HRS AND REPLACEMENT REQUIRED W/I 350F HRS. ENGINE RUN AND LEAK CHECK OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,998 hrs · 50,064 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 66,998 hrs · 50,064 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31-35 OF THE CABIN WERE INOPERATIVE. MAINTENANCE CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: LIGHT — INOPERATIVE (SEAT 35) · airframe 66,817 hrs · 49,919 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 35 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: LANYARD — DAMAGED (L1 DOOR SLIDE) · airframe 65,037 hrs · 48,734 cycles

MAINTENANCE FOUND SLIDE LANYARD AT THE L1 DOOR FREYED AND DAMAGED. MAINTENANCE REPLACED SLIDE LANYARD ASSY AT L-1 DOOR. CKS OK.

Part: RIB — CRACKED (RT WING LE) · airframe 64,578 hrs · 48,456 cycles

CRACK ON RIB XRS=164.000 L/E RT WING. RIB WAS REPAIRED IAW SRM 57-06-B, PAR-16.

Part: OUTFLOW VALVE — LEAKING (CABIN PRESSURE) · airframe 63,722 hrs · 47,852 cycles

FLIGHT DIVERTED DUE TO THE LOSS OF CABIN PRESSURE CONTROL. AN EMERGENCY WAS DECLARED. MAINTENANCE DISCOVERED THAT THE OUTFLOW VALVE WAS LEAKING BEYOND ALLOWABLE LIMITS AND PLACED IT ON MEL 21-00-25. THE OUTFLOW VALVE WAS REPLACED AND 2 OTHER FUSELAGE LEAKS WERE FOUND AND SEALED. THE ACFT HAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,873 hrs · 47,254 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY EMERGENCY POWER SUPPLY IAW AMM 33-53-00. OPS CHECKED OK. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,740 hrs · 47,178 cycles

DURING LINE CHECK, NOTED AFT WING ENERGENCY DOOR UPPER LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-50 AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,627 hrs · 46,354 cycles

DURING LINE CHECK, MX FOUND THAT BOTH OF THE OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: HEATER BLANKET — DAMAGED (RT WING) · airframe 60,965 hrs · 45,858 cycles

CRACK AFT EDGE ON RT WING HEATER BLANKET. RT WING HEATER BLANKET PANEL WAS REPLACED DUE TO DIMENTIONS OF DAMAGE (0.656") IAW AMM 30-80-02, PAGE BLOCK 401 PARA 2A. RII COMPLETED BY INSPECTION STAMP INSPECTOR.

Part: FLOORBEAM — CORRODED (BS 1309) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON FLOORBEAM ANGLE BS 1309 X=-20. CORROSION WAS REMOVED IAW SRM 51-10-3 OAR 26 MEASURED AND FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. REPAIRED IAW ER/A 514805-14 REV ORIGINAL.

Part: SKIN — CRACKED (BS 1418) · airframe 60,965 hrs · 45,858 cycles

CRACK ON FUSELAGE SKIN AT STA Y=1418 BETWEEN LONGERON 2 AND 3LT WITH A LENGTH OF 0.593 INCH. CRACK REMOVED, REPAIR DOUBLERS & FILLERS WERE FABRICATED AND INSTALLED IAW ER/A 514799-14AD REV ORIGINAL. REPAIR WAS IDENTIFIED IAW PS 900-5-1, NR 4.

Part: CARGO TRACK — CORRODED (BS 1007-1222) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 1007-1222 ALSO ON SPLICE AT AFT CARGO COMPARTMENT. LT CARGO TRACK OUT OF LIMITS WAS REPLACED IAW SRM 51-30-2 AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (BS 1136-1212) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON FLOOR SUPPORT FROM BS 1212 TO 1136 ABOVE LONGERON 29R. CORROSION WAS REMOVED, FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. FLOOR SUPPORT REPLACED IAW DWG 593660, REV BZ AND SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1361C. CORROSION WAS REMOVED, COUNTERSINK WERE MEASURED AND WERE FOUND OUT OF LIMITS. CONDITION II MAXIMUM DIAMETER ALLOWABLE IS 0.554", 0.585", 0.554", 0.567", AND 0.0602". THEREFORE ACCESS PLATE WAS REPLACED, CORROSION 2.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 60,965 hrs · 45,858 cycles

DENT ON LT ELEVATOR LOWER SKIN STA XE 219 6" LENGHT 2.437 WITH REF ONRC 702. DENT OUT OF LIMITS IAW SRM 51-50-2, PARA 5. DENT WAS REPAIRED IAW SRM 55-01, FIG 2 AND 51-60-0 PARA 5. REMOVE FROM MONITOR. DENT REPAIR IS PERMANENT.

Part: PLATE — CORRODED (BS 1238-1260) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LONGERON PLATE 23LT BETWEEN STA Y=1238 TO 1260. UTILITARY TUNNEL AFT CARGO COMPARTMENT. STRIP WAS REMOVED AND A NEW STRIP WAS INTALLED IAW SRM 59300-2, REV EH.

Part: CARGO TRACK — CORRODED (BS 1022-1322) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LT CARGO TRACK FROM BS 1022 TO 1322 AT AFT CARGO COMPARTMENT. LEFT CARGO TRACK OUT OF LIMITS AND WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON TIE TRACK FROM BS 1212 - 1322 AT AFT CARGO COMPARTMENT. REMOVED CARGO TRACK AND INSTALLED NEW CARGO TRACK IAW SRM 51-30-1 AND 51-10-4, 51-10-3, PAR 18 AND 21.

Part: CARGO TRACK — CORRODED (BS 1138-1155) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION AND ELONGATED HOLES ON RT CARGO TRACK BETWEEN STA Y=1138-1155 AT AFT CARGO COMPARTMENT. REMOVE CARGO TRACK AND CORROSION, MEASURE, REPLACED CARGO TRACK, AND INSTALLED NEW CARGO TRACK IAW SRM 51-10-3, PAR 14, 21, 26, 38, 53,-05 FIG 4C, 51-30-2,51-30-1, 51-30-5.

Part: LONGERON SPLICE — DAMAGED (BS 1155-1174) · airframe 60,965 hrs · 45,858 cycles

CRACK ON REPAIR SPLICE LONGERON 23LT BETWEEN STA Y=1155 TO Y=1174, UTILITARY TUNNEL AFT CARGO COMPARTMENT. REMOVE SPLICE, FABRICATE, AND INSTALL NEW SPLICE IAW SRM 51-10-3, PAR 21, 14 AND ER/A 269449-14, REV B.

Part: DOUBLER — CORRODED (BS 1338) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON PRODUCTION DOUBLER BELOW VERTICAL WEB, STA 1338 BETWEEN LONG 28RT-28LT AT AFT CARGO COMPARTMENT. DUE TO EXCESIVE CORROSION ON PRODUCTION DOUBLER IT WAS REPLACED IAW DWG 9915561, REV CG AND SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LONGERON 22L BETWEEN BS 1287 TO 1309, ALSO RUSTED NUTS SAME AREA LT UTILITARY TUNNEL AFT CARGO COMPARTMENT. CORROSION ON LONGERON WAS REMOVED AND REMAINING THICKNESS WAS FOUND OUT OF LIMITS IAW SRM 53-01, FIG 61. SECTION OF LONGERON FROM BS 1279 TO 1338 WAS REPLACED IAW SRM 53-02, FIG 18 WITH A NEW SECTION OF LONGERON AND REPAIR SPLICE, ALSO NUTS SAME AREA WERE REPLACED IAW SRM 51-30-5.

Part: PLATE — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LONGERON PLATE 23L BETWEEN BS 1287 TO 1309 UTILITARY TUNNEL AT AFT CARGO COMPARTMENT. STRIP WAS REMOVED, NEW STRIP WAS REPLACED IAW SRM 51-30-2.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LOWER BEAM OF AFT CARGO COMPARTMENT DOOR FRAME BS 1155 TO 1212. CORROSION ON LOWER BEAM WAS REMOVED, MEASURED, AND FOUND OUT OF LIMITS. REPAIR WAS INSTALLED IAW SRM 53-05, FIG 1, 2, 3, 51-10-3, PAR 14, 21, 26.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LONGERON 27L BETWEEN BS 1287-1309. REPAIR SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437 L4R) · airframe 60,965 hrs · 45,858 cycles

CRACKED LONGERON 4R BS 1437 IN AFT ACCESSORY COMPARTMENT. DAMAGED SECTION LONGERON WAS REMOVED AND NEW SECTION LONGERON WAS INSTALLED IAW SRM 53-02, FIG 2.

Part: LONGERON — DAMAGED (BS 1309) · airframe 60,965 hrs · 45,858 cycles

ELONGATED SCREW HOLE ON LONGERON 29R BS 1309. LONGERON SECTION BS 1278 -1338 WAS REMOVED AND A NEW LONGERON SECTION WAS INSTALLED IAW SRM 51-30-2 AND A NEW SPLICE WAS INSTALLED IAW SRM 53-02, FIG 18.

Part: LONGERON — DAMAGED (BS 1309) · airframe 60,965 hrs · 45,858 cycles

ELONGATED SCREW HOLES ON LONGERON 29L BS 1309. LONGERON SECTION ON STA Y=1282 TO Y=1338 WAS REMOVED, FABRICATED, AND INSTALLED IAW SRM 53-02, FIG 18.

Part: DOUBLER — CRACKED (BS 423) · airframe 60,965 hrs · 45,858 cycles

CRACK ON INTERNAL DOUBLER AT THE LOWER AFT DOOR FRAME CORNER BS 423.5 BETWEEN L26 - 27R OF THE FWD CARGO COMPARTMENT. IDENTIFIED CRACK ON PRODUCTION DOUBLER AND TRIMMED OUT FABRICATED REPAIR PARTS AND PERFORMED REPAIR IAW SRM 53-05, FIG 105 WITH DOUBLER, TRIPPLER, AND REPAIR FILLERS SOME MATERIAL ORIGINAL. RII COMPLETED BY INSPECTION.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER CUSP WEB BETWEEN STA -44 TO -60 Y=655-674, 674-693 AND 636-655 (MRB 53-037-01) REF (T0 282332) (CARD 193 ZONE 58). CUSP WEB FROM STA 598 TO 712 WAS REMOVED WITH ALL ITEMS WITH THEM, (GUSSETS, FLOOR SUPPORTS) NEW CUSP WEB WAS INSTALLED (WITH -ITEMS REMOVED FOR FACILITY ACTIVITIES) IAW MD-88 51-30-2, SRM 51-30-5. (LP 0903279)

Part: LONGERON — CRACKED (BS 1437 L3R) · airframe 60,965 hrs · 45,858 cycles

CRACKED LONGERON 3R, BS 1437 . DAMAGED LONGERON REMOVED, NEW SECTION LONGERON WAS INSTALLED IAW SRM 53-02, FIG 1.

Part: LONGERON — CORRODED (BS 1287-1338) · airframe 60,965 hrs · 45,858 cycles

CORROSION ON LONGERON SPLICE 30 FROM BS 1287 TO 1338 AT AFT CARGO COMPARTMENT. DAMAGED SECTION OF LONGERON WAS REMOVED IAW SRM 51-30-2, NEW SECTION INSTALLED IAW SRM 51-30-5, 51-30-2.

Part: LONGERON — CRACKED (BS 1380 L13L) · airframe 60,965 hrs · 45,858 cycles

CRACKED LONGERON 13LT AT STA Y=1380 AT AFT ACCESSORY COMPARTMENT REF (T0 283086) (CARD 580, ZONE 59) DAMAGED SECTION LONGERON WAS REMOVED, PREVIOUS REPAIR SPLICE WAS REMOVED, NEW SECTION LONGERON WAS DRILLED & ADJUSTED, NEW LONGERON SECTION & PREVIOUS REPAIR SPLICE WERE INSTALLED IAW SRM 53-02, FIG 18. RII COMPLETED BY INSPECTION STAMP INSPECTOR IAC 200802798 AM DELTA ID 872769.

Part: LONGERON — CRACKED (BS 1418 L2L) · airframe 60,965 hrs · 45,858 cycles

CRACKED LONGERON 2L BS 1418 AFT ACCESSORY COMPARTMENT. DAMAGED SECTION LONGERON REMOVED, NEW LONGERON SPLICE WAS INSTALLED IAW SRM 53-02 FIG. 18.

Part: LONGERON — CRACKED (BS 905 L4L) · airframe 60,965 hrs · 45,858 cycles

CRACKED LONGERON 4L BS 905. DAMAGED SECTION LONGERON WAS REMOVED AND NEW SECTION WAS INSTALLED WITH REPAIR PARTS IAW SRM 53-02, FIG 18.

Part: SKIN — DAMAGED (RUDDER) · airframe 60,965 hrs · 45,858 cycles

DURING HEAVY MX CHECK, THE RUDDER WAS NOTED TO HAVE DAMAGE TO THE SKIN. DAMAGE REPAIRED IAW SRM 51-70-1AD, PARAGRAPH 23.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,965 hrs · 45,858 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AT LT CUSP WEB BETWEEN STA X=54-60, Y=917-925. REF MBR 5300-2586. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-1 .

Part: STRUCTURE — WORN (TAILCONE RELEASE) · airframe 60,965 hrs · 45,858 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CAM BASE WAS WORN AT AFT OF ACCESSORY COMPARTMENT AT 1100 POSITION. THE BASE WAS REPLACED.

Part: LONGERON — DAMAGED (BS 160) · airframe 60,965 hrs · 45,858 cycles

CRACKED LONGERON 4L AT BS 160 AT FUSELAGE STRUCTURE. DAMAGE LONGERON WAS REPLACED AND INSTALLED IAW SRM 53-02 AND 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 1174) · airframe 60,965 hrs · 45,858 cycles

CRACKED FRAME ON STA Y=1174 BTW LONGERON 5LT AND 7LT AT PAX CABIN. CRACKED FRAME WAS REPAIR FABRICATED DOUBLER, TREATED AND PAINTED AND INSTALLED PARTS OF REPAIR IAW ER/A 495237-14MA, REV ORIG ASSOCIATED ER/A 49-523714 ADDED FOR AC 0950.

Part: LONGERON — CRACKED · airframe 60,965 hrs · 45,858 cycles

CRACK ON LONGERON 4L AT BS 160. REPAIRED IAW SRM 53-02 FIG 18.

Part: SUPPORT — CRACKED (BS 941) · airframe 60,965 hrs · 45,858 cycles

CRACKED SUPPORT ON BS 941 AND X=-25 AT RT MAIN GEAR WHEEL WELL. SUPPORT WAS REPLACED IAW EA 09-076074-03 ME-02.

Part: LONGERON — CRACKED (BS 1437) · airframe 60,965 hrs · 45,858 cycles

CRACKED LONGERON 3L BS 1437 AT AFT ACCESSORY COMPARTMENT. DAMAGED SECTION WAS REMOVED, NEW LONGERON WAS FABRICATED, AND REPAIR LONGERON SPLICE WAS INSTALLED IAW SRM 53-02, FIG 18.

Part: SKIN — DENTED (BS 247 L18-19L) · airframe 60,965 hrs · 45,858 cycles

DENT ON FUSELAGE SKIN BS 247 AND L18-19L. DENT FOUND OUT OF LIMITS. IAW ER/A 273527-14 REV. "A".

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 60,746 hrs · 45,712 cycles

DURING OVERNIGHT MX, THE EMERGENCY ESCAPE AISLE PATH LIGHTS AT SEAT 36D WERE FOUND TO BE INOPERATIVE. MX RETERMINATED THE SEAT WIRING HARNESS AND OPS CHECKED THE EMERGENCY LIGHT SYS IAW AMM 33-53 AND OPS CHECKED GOOD,

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,408 hrs · 45,465 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 31 IN THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,159 hrs · 45,287 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROWS 11-14 AND ROWS 22-25 WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,746 hrs · 43,633 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-38 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 57,694 hrs · 43,602 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 32-35 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 57,604 hrs · 43,541 cycles

WHILE ACCOMPLISHING THE REPAIR TO THE SUBJECT VERTICAL STABILIZER IAW EA 09-470871-12 MAINT FOUND 3 HOLES ON THE LOWER LT AND 6 LOWER RT SIDE OF PANEL THAT WERE ALSO OVERSIZED. REPAIR ERA 498068-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,604 hrs · 43,541 cycles

STA 1463 CANTED FRAME WEB ABOVE L9L FOUND CRACKED FROM FASTENER HOLE ON -53 WEB. REPAIRED PER ERA 498041-14.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 57,604 hrs · 43,541 cycles

CRACKS WERE FOUND ON THE FUSELAGE TO VERTICAL STABILIZER. ATTACH ANGLE NEAR STATION 1465. REPAIR IAW ERA 498016-14.

Part: WIRE — BROKEN (CABIN) · airframe 57,604 hrs · 43,541 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 1C IN THE FIRST CLASS CABIN, WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR AND WILL RE-PIN IT WHEN PARTS BECOME AVAILABLE. THE SYSTEM HAS NOT RETURNED TO NORMAL OPERATION AS OF 21NOV11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,119 hrs · 43,209 cycles

DURING LINE CHECK MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHTBETWEEN ROW 17 AND 23 INOPERATIVE. MAINTENANCE RE-LAMPED AND REPLACED BATTERIES AT BATTERY PACK B5-102. OPERATION OF LIGHTS NOW CHECKS OK.

Part: BOTTLE — DISCHARGED (EVAC SLIDE) · airframe 56,415 hrs · 42,692 cycles

DURING LINE CHECK MAINTENANCE FOUND R1 DOOR SLIDE BOTTLE OUT OF LIMITS. MAINTENANCE REPLACED SLIDE ASSEMBLY PER MD88 AMM 25-62-201. AIRCRAFT IS OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,210 hrs · 42,540 cycles

DURING LINE CHECK, MAINTENANCE FOUND TAIL CONE EMERGENCY PATHWAY LIGHTS AND AFT CABIN EXIT DOOR SIGNS INOPERATIVE. MAINTENANCE FOUND THE BATTERY POWER SUPPLY B5-212 TO BE BAD AND REPLACED IT. OPERATION CHECKS GOOD.

Part: SKIN — DAMAGED (BS 731) · airframe 56,188 hrs · 42,527 cycles

THE FUSELAGE SKIN WAS FOUND BULGED AND CRACKED AROUND THE ANTENNA CUTOUT FS 719, L30. REPAIRED IAW ERA 481174-14, REV A.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 55,613 hrs · 42,167 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING INOPERATIVE FROM ROW 31 TO 38. MX REPAIRED THE WIRING AND REPLACED THE ASSOCIATED FUSE IN THE BATTERY PACK. OPS CK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,751 hrs · 41,588 cycles

DURING LINE CHECK MX, FOUND AFT EMERGENCY LIGHTS INOPERATIVE. MX REPLACED BATTERY AND CHARGER AT BS-212 STA 1233 IAW AMM. OPERATION OF LIGHTS NOW CHECKS OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,704 hrs · 41,562 cycles

DURING LINE CHECK, MX FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT AND L2 DOOR INOPERATIVE. MX REPLACED BATTERY IN AFT LAVATORY CEILING AND FUSE IN POWER SUPPLY R5-212. OPS OF LIGHTS NOW CHECK OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 54,459 hrs · 41,390 cycles

MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 22DE TO BE INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR AT THE LIGHT ASSEMBLY. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (ODI 2010-D0941) (DLM88102028).

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,135 hrs · 41,175 cycles

MX FOUND THE AFT EMERGENCY LIGHTS FROM THE AFT STAIRS TO BE INOPERATIVE. MX FOUND THE FUSE BAD ON THE BATTERY PACK CONTROLLER. MX REPLACED THE FUSE. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 54,099 hrs · 41,150 cycles

MX FOUND THE EMERGENCY PATH LIGHTS AT 30DE TO BE INOPERATIVE. MX FOUND BROKEN WIRES AND SPLICED IN CONNECTORS. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: SPAR CAP — CRACKED (RT WING) · airframe 53,862 hrs · 40,968 cycles

RT WING MAIN FRAME LOWER REAR SPAR CAP XRS-164 CRACK REPAIR IAW ERA 481554-14

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 53,830 hrs · 40,945 cycles

MX FOUND THAT THE AFT SERVICE DOOR AND AFT STAIRWELL EMERGENCY LIGHTS WERE INOPERATIVE. MX FOUND A BAD FUSE ON THE EMERGENCY BATTERY PACK. MX REPLACED THE FUSE AND THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,685 hrs · 40,846 cycles

EMERGENCY LIGHTS INOP AT PAX SEATS 31-38. REMOVED AND REPLACED BATTERY PACK AND CHARGER FOR ROWS 31-38 SEAT LIGHTS. REMOVED AND REPLACED AFT PWR SUPPLY ISOLATION DIODE PER MD-88 SWPM. RELAMPED ROWS 31-38. ALL OPS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,490 hrs · 40,729 cycles

FOUND AISLE EMERGENCY LIGHT SECTION 4 INOP. R & R BATTERY CHARGER AT THE SAME LOCATION IAW AMM. CKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,463 hrs · 40,717 cycles

ON L/O CK FOUND ALL EMERGENCY LIGHTS INOP AFT OF SEAT ROW 30. REPLACED PWR SUPPLY AND BATTERY. LIGHTS CK OK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 52,855 hrs · 40,354 cycles

EMERGENCY LIGHT IN FLOOR INOP ROWS 31-38. CLOSET FWD OF GALLEY OG4 EMER LIGHTS IN FLOOR INOP ROWS 31-38. REPLACED POWER SUPPLY AND BATTERY, OPN NOW CHECKS GOOD.

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 52,627 hrs · 40,188 cycles

COMPLY WITH EA 09-460214-12AD RT HORIZONTAL STABILIZER CAP SPLICE PER SERVICE REWORK DWG SR09550027.

Part: BALLAST — DAMAGED (CABIN) · airframe 52,166 hrs · 39,861 cycles

UPON LANDING IN ATL AFTER ARRIVAL AT GATE WITH DOOR OPEN. SMELLED STRONG ACRID ODOR AGAIN IN 1ST CLASS GALLEY ENTRY DOOR AREA. FOUND BALLAST'S AND HARNESS'S AT SEAT'S 3/4 AB SHORTED AND MELTED.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (LEFT) · airframe 49,211 hrs · 37,945 cycles

ON DESCENT 27000 FT, THE LEFT HYD PRESS LOW ANNUC CAME ON, DROPPED TO ZERO PSI AND QUANT INCREASED LEFT REV WOULD NOT STOW AFTER LANDING. FOUND LT SYSTEM RESERVOIR ACCUMMULATOR FULL OF AIR BLED AIR FROM RESERVOIR. OPS CHK GOOD QTY, NO LEAKS NOTED. CYCLED FLT CONTROLS PRESS NORMAL. NO LEAKS NOTED PRESS NML. NO HISTORY.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 47,188 hrs · 36,626 cycles

HYD LOSS ON TOP OF DESCENT DURING FLAP EXTENSION. TIGHTENED B-NUT IN RT WHEEL WELL. SERVICED HYD FAN MOTORS A HYD PUMPS LK CKS GOOD. CYCLED FLIGHT CONTROLS CKS OK.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

EXFOLIATION CORROSION ON LT CUSP WEB FROM STA Y=1174 TO Y=1193, TASK 46-53305. REPAIRED PER ERA 398191-14MA ON N/R T0063373 AT HMV-3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

CRACK ON RT CUSP WEB AT STA Y=807 TASK CARD 58-533139 IN PAX CABIN. REPAIRED PER ERA 398191-14MA ON N/R TOO63499 AT HMV-3.

Part: STIFFENER — BROKEN (BS 1474 L22-23L) · airframe 47,008 hrs · 36,501 cycles

BROKEN STIFFENER ON STA 1474 CANT BETWEEN LONG 22 AND 23 LT. STIFFENER REPLACED PER DWG 9911946.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 47,008 hrs · 36,501 cycles

CRACKED LT FWD UPPER FACE P-DOME ANGLE BETWEEN LONGERONS 3 AND 4 LT. REPAIRED PER DWG 9915562 REV P ON N/R TOO63359 AT HMV-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

GENERAL CORROSION ON RT CUSP WEB STA Y=1030 TO Y=1036, 1045 TO 1058 AND 1064 TO 1075 TASK CARD 58-53313. REPAIRED PER ERA 398191-14MA ON N/R T0062851 AT HMV-3.

Part: ANGLE — CORRODED (BULKHEAD) · airframe 47,008 hrs · 36,501 cycles

EXFOLIATION CORROSION ON AFT PRESSURE DOME 'T' EXTRUSION. TASK CARD 57-53300/57-53301. "T" REPLACED PER DWG 5910130 AT STA 1338,X=0 ON N/R T0063245 AT HMV-3.

Part: FLOORBEAM — CRACKED (FUSLEAGE) · airframe 47,008 hrs · 36,501 cycles

FOUND CRACKED FLOOR SUPPORT AT STATION Y=905, X =42. REPAIRED PER DWG 9923417 ON N/R T0062835 AT HMV-3.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

CRACKED FRAME AT FLOORBEAM JOINT STA Y=864 X=56. REPAIRED PER DWG SR 09530282 ON N/R T0062703 AT HMV-3.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

PUNCTURE ON LT CUSP WEB AT STA Y=986. REPAIRED PER ERA 398191-14MA.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

PUNCTURED ON LT CUSP WEB AT STA Y=819, REPAIRED PER ERA 398191-14MA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

FOUND CRACK ON LT CUSP WEB AT STA Y=226, REPAIRED PER ERA 398191-14 MA REV A.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

EXFOLIATION CORROSION ON LT CUSP WEB AT STA Y=910 TO 921. REPAIRED PER ERA 398191-14MA REVA.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

FOUND CRACK ON LT CUSP WEB AT STA Y=703. REPAIRED PER ERA 398191-14MA REV A.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 47,008 hrs · 36,501 cycles

CRACKED RT CUSP WEB AT STA Y=218, REPLACED WEB.

Part: VANE — MISREPAIRED (LT TE FLAP) · airframe 47,008 hrs · 36,501 cycles

UNSUITABLE REPAIR ON LT INBD FLAP INBD GUIDE VANE. REPAIRED PER SRM 57-03D.

Part: SKIN — BULGED (BS 629 LBL 5) · airframe 47,008 hrs · 36,501 cycles

FUSELAGE SKIN BULGED WITH A 1/4 IN CRACK STA 629 LBL 5. REPAIRED PER SRM 53-04D.

Part: B-NUT — LOOSE (BRAKE LINE) · airframe 44,027 hrs · 34,369 cycles

ON DESENT INTO SRQ GOT RT HYD QTY LOW LIGHT AND QTY DOWN TO 3 QTS RT PRESS OK. COMPLIED WITH QRH HYD QTY LOW PROCEDURE AND QTY WENT TO 17 QTS. SUSPECTED FORMING, PRIOR TO LANDING WITH FLUID REMAINING IAW QRH TURNED BOTH PUMPS ON AND QTY WENT TO 3 QTS AGAIN. RT PRESS OK. LOWERED LDG GEAR AND FLAPS. FOUND NR 4 BRAKE LINE ON AN B-NUT LOOSE. SECURED SAME, SERVICED RT HYD SYSTEM TO FULL. LEAK CHECK OK. AUX PUMP OK. RT EDP WILL NOT PROVIDE PRESSURE. CHECKED RT EDP FOR DAMAGE, NONE FOUND. RAN AND BLED RT EDP, PRESS CKS GOOD.

Part: CARTRIDGE — MISSING (EXTINGUISHER) · airframe 43,656 hrs · 34,111 cycles

H2O FIRE EXTINGUISHER SEALED WITH DELTA IMPRINT ON BOARD, FLT ATTENDANT NOTICED THROUGH HANDLE THAT THERE WAS NO CO2 CART. INSTALLED DPN D263701217 S/N OFF 12231. REPLACED EXTINGUISHER.

Part: COMPRESSOR — FAILED (POTABLE WATER) · airframe 41,748 hrs · 32,740 cycles

AT FL 340 CRUISE FLIGHT COCKPIT DETECTED ELECTRICAL SMELL. REPLACED FAILED POTABLE WATER SYSTEM COMPRESSOR.

Part: GENERATOR — FAILED (NR 1 ENGINE) · airframe 41,193 hrs · 32,343 cycles

ON DEPARTURE FROM DCA LEFT GENERATOR FAILED WITH NO VOLTS OR FREQS CAUSING CROSSTIE LOCKOUT. REPLACED LEFT CSD AND GENERATOR.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 34,040 hrs · 27,273 cycles

EMERGENCY LIGHTS INOP AFT OF ROW 31. REPLACED POWER SUPPLY NOW CHECK NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 33,969 hrs · 27,221 cycles

AFT CABIN EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, CHECKS GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 33,713 hrs · 27,013 cycles

EMERGENCY ESCAPE PATH LIGHTS INOP FROM 31DE AFT INCLUDING TAIL COMPARTMENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,226 hrs · 26,625 cycles

DURING HMV-2 A DENT WAS NOTICED AT FS 89.050 BETWEEN L18R AND L19R. DENT WAS CUT OUT AND AN INTERNAL REPAIR INSTALLED PER ERA 412359-14.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,226 hrs · 26,625 cycles

DURING HMV-2, CORROSION ON THE C2 DOORWAY JAMB BEAM WAS NOTED AT THE DOOR STOP FITTING HOLES. ALSO, ALONG THE HORIZ FLANGE OF THE BEAM. THERE WAS AN EXISTING SRM REPAIR WHICH WAS REMOVED. DAMAGE WAS REMOVED, CLEANED UP AND A REPAIR INSTALLED PER ERA 412362-14, REV A.

Part: STRUT — LOW (NLG) · airframe 32,829 hrs · 26,323 cycles

AFTER TAKEOFF NOSE GEAR WOULD NOT SHOW UP AND LOCKED. SERVICED NOSE STRUT TO PROPER LEVEL.

Part: BLADE — DAMAGED (NR1 ENGINE) · airframe 30,631 hrs · 24,598 cycles

ENCOUNTERED WINDSHEAR ON APPROACH TO TPA. HIT TOGA BUTTONS AND BEGAN CLIMB. HEARD LOUD THUMP WHEN POWER CAME UP ON LEFT ENGINE. LEFT ENGINE PRODUCED NO EPR FOR REMAINDER OF FLIGHT. FOUND BLADE DAMAGE. REPLACED ENGINE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,354 hrs · 24,394 cycles

FUSELAGE / SKIN / FS 780 / STRG. 29R-30 : CORROSION REPAIR. AN AREA OF CORROSION WAS FOUND ON THE FUSELAGE SKIN AT FS 780, BETWEEN STRINGERS 29R AND 30 NEAR AN ANTENNA CUTOUT. THE CORRODED AREA WAS REMOVED WITH A 7" X 5.25" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 379342-14, REV A.

Part: AFCS — FAILED (E/E BAY) · airframe 28,633 hrs · 23,107 cycles

AFTER TAKEOFF, F/O AIRSPEED FAILED, CAPT AND F/O MAP FAILED. ATS AND AUTO PILOT DISCONNECTED. REPLACED NUMBER 2 CADC.

Part: AIR DISTRIBUTION — ODOR (CABIN)

SMOKE ALARM WENT OFF ON LANDING IN RT AFT LAV. F/A REPORT SMELLING A HOT OILY SMELL IN REAR OF A/C. RAN PACKS WITH APU AND ENG BLEED AIR INSP OPS OF PACKS AND ENG BLEED SYS, NO SMOKE OR SMELL OBSERVED. INSP LAVS FOR PROBLEMS, ALL OK. INSP 48 SECTION FOR LEAKS ALL OK.

Part: VALVE — MALFUNCTION (AIRFOIL DE-ICE)

DURING FINAL APPROACH AFT CABIN HAD SLIGHT SMOKE SMELL BOTH SMOKE DETECTOR IN LAVS WENT OFF. BY LANDING SMELL HAD CEASED, ALARMS HAD STOPPED. REPLACED AIRFOIL PRESS REG VLV, RAN ENGS, PACKS AND ANTI-ICE SYSTEMS. PERFORMED AUG VLV CK PER PFHB. NO SMOKE AND NO ODOR.

Part: WINDOW — POPPED IN (COCKPIT)

ON APPROACH, CAPT SLIDING WINDOW POPPED IN, DUMPING CABIN PRESSURIZATION. REPLACED CAPT SLIDING WINDSHIELD, NO DAMAGE TO THE TRACKS OR SEAL.

Part: ACM — LOW OIL (LEFT)

ON FINAL APPROACH, BLUE SMOKE BEGAN TO FILL BOTH CABIN AND COCKPIT. ENGINE AND FOIL ANTI-ICE WERE ON, APU WAS OFF AND SMOKE DETECTORS WENT OFF. FOUND LEFT HAND ACM OIL LEVEL LOW, LEFT PACK INOP PER MEL.

Part: SKIN — DENTED (FS 237)

THE FUSELAGE SKIN WAS FOUND TO BE BADLY DENTED AROUND FS 237 BETWEEN 18L AND 20L. THE DENT WAS CUT OUT AND A FILLER AND DOUBLER WAS INSTALLED PER DL ERA 273527.

Part: SKIN — PUNCTURED (BS 207-215)

SKIN PUNCTURE ON RT SIDE EXTENDING FROM FS 207 TO FS 215 AND FROM LONGERON 19 TO 20. GROUND DAMAGE REPAIRED PER DL ERA 2715008-14.

Part: BRACKETS — CRACKED (CARGO DOOR)

OUTER DOOR WILL NOT LATCH IN UPLOCK POS, BOTH BRACKETS DAMAGED AND CRACKED. CRACK ALSO, IN AFT EDGE OF DOOR BELOW AFT HANGER. FOUND DURING F-1 LETTER CK TPAMM 3/2/95. REPAIRED FIRST ITEM BY SRM 52-05 FIG 27, REPAIRED 2ND ITEM BY SRM 52-05 FIG 26A.