N922DL

Part: FRAME — CRACKED (BS 1310) · airframe 79,191 hrs · 60,344 cycles

CRACK- 1310 CANT FRAME CRACKED AT TAIL CONE GUIDE PIN 4 OCLOCK POSITION. REMOVED DAMAGED FRAME PN 5966769U501. (458779) DRILLED NEW FRAME AND BEGAN INSTALLATION PER BOEING DWG 5966769. COMPLETED INSTALLATION OF FRAME PER BOEING DWG 5966769. (LP0863490)

Part: BRACKET — OUT OF ADJUST (CABIN) · airframe 78,275 hrs · 59,521 cycles

EMERGENCY SEAT ISLE LIGHT INOP AT SEAT 31 DE. ADJUSTED BRACKET AND BULB FIXTURE AT ISLE SEAT 31 DE. OPS CK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,811 hrs · 59,995 cycles

FUSELAGE SKIN, STA 750, L-30 CORROSION REPAIR, PERMANENT REPAIR. C/W ERA 455233-14 REV C, MON CLOSED.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 77,477 hrs · 58,862 cycles

FIRST OFFICER'S EMERGENCY ESCAPE WINDOW WILL NOT OPEN. ADJUSTED THE WINDOW IAW AMM 56-10. OPS CHECKED GOOD.

Part: NUT — LOOSE (OIL FILTER) · airframe 77,459 hrs · 58,850 cycles

AT FL330 MASTER CAUTION LOW OIL PRESS RIGHT ENG. RAN QRH, 0 QUANTITY, THEN SHUT DOWN R ENGINE. R PRESSURE AND QUANTITY BOTH 0. WINDMILL 15 MINUTES. UPON ARRIVAL FOUND LOWER COWL COVERED WITH OIL. FOUND LOOSE STUD/NUT ON OIL FILTER CAP W/O-RING PROTRUDING. WIP DC 611518. REPLACED NUMBER 2 ENGINE ON A/C LOG 0477901.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,287 hrs · 58,710 cycles

EMERGENCY LIGHT AT SEAT 20 DE INOPERATIVE. REPLACED THE SEAT WIRE HARNESS IAW AMM 33-52. CHECKED GOOD.

Part: PANEL — CORRODED (HEATER BLANKET) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON RT HEATER BLANKET AROUND ACCESS NR 1410C CUT OUT (AD). LEVEL CORROSION 2. RT HEATER BLANKET PANEL WAS REPLACED PER AMM 30-80-02-401 BLOCK 401. OVERWING HEATER BLANKET FUNCTIONAL TEST WAS PERFORMED PER AMM 30-80-02-0501. TEST OK.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 76,246 hrs · 57,890 cycles

AWR HIDDEN DAMAGE: ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT. ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT WERE REPAIRED PER ETI-88-17-235 REV 3 AND ER/A 560942-14 REV ORG.

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON SPACER AT MID CARGO COMPARTMENT DOOR JAMB BEAM REPAIR ALSO THE REPAIR DOES NOT MEET REQUIREMENTS PER SRM (SM) (C2) (IN REF AMDS 5300-2358). SPACER AT MID CARGO COMPARTMENT DOOR JAMB BEAM REPAIR ALSO THE REPAIR DOES NOT MEET REQUIREMENTS PER SRM, WERE REPLACED AND REPAIRED PER SRM 53-05 FIG 123.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 76,246 hrs · 57,890 cycles

LOW PRESSURE ON THE R1 SLIDE. THE R1 SLIDE WAS REPLACED IAW AMM 52-62-00.

Part: ANGLE — CORRODED (BS 218-227) · airframe 76,246 hrs · 57,890 cycles

AWR.HIDDEN DAMAGE:THIS CARD IS ISSUED WITH THE CORRECT TEXT INSTEAD OF NRC 00805. CORROSION ON LH CUSP ANGLE BTW STA Y=218 TO Y=- 227 AND X=54 TO X=60 AT CABIN FLOOR STRUCTURE. PERMANENT REPAIR ON ANGLE CUSP WAS ACCOMPLISHED PER ETI-88-17-228 REV. 2. AND ER/A 560908-14 REV. ORG. (LP0210056)

Part: LONGERON SPLICE — CRACKED (BS 1271-1287) · airframe 76,246 hrs · 57,890 cycles

CRACKED LONGERON SPLICE 22L BETWEEN BS 1271 TO 1287. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 53-02, FIG.18, 51-30-5, 51-10-3, & 51-10-4.

Part: ANGLE — CORRODED (BS 1231) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON CEILING SUPPORT ANGLE BS 1231, LBL 18 AND 32 IN THE AFT CARGO BAY. THE ANGLE WAS REPLACED IAW DWG 5956707, REV AT, SRM 51-10-3, 51-10-2, 51-10-4, 51-30-2, AND 51-30-5.

Part: BULKHEAD — CORRODED · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON AFT BULKHEAD AT WALKING BRIDGE. THE BULKHEAD WAS REPLACED IAW SRM 51-30-2 AND DWG 9911993 REV CJ.

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON INTERCOSTAL AT WALKING BRIDGE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON THE LT WING HEATER BLANKET FWD FUEL BOOST PUMP SECONDARY ACCESS COVER. FWD FUEL BOOST PUMP SECONDARY ACCESS COVER WAS REPLACED.

Part: FLOOR SUPPORT — DAMAGED (BS 1287-1307) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

FLOOR SUPPORT CORRODED AND CRACKED, BS 1287 TO 1307, BL 0. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIG 4.

Part: DOOR FRAME — WORN (LT MLG WW) · airframe 76,246 hrs · 57,890 cycles

WORN LEFT MLG WW DOOR FRAME AFT CHANNEL BS 937 AND LBL 60. MLG WW DOOR FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, SRM 51-10-04 , AND 51-10-3 PAR 14, 21.

Part: SEAT TRACK — CORRODED (BS 790-796) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION OUT OF LIMIT ON THE SEAT TRACK RBL 54, BS 790 - 796. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIG 4F, 51-10-03, PAR 21, 14, AND 51-30-01.

Part: SUPPORT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON GIRT BAR SUPPORTS AT FWD GALLEY SERVICE ENTRACE DOOR. SUPPORTS AT FWD GALLEY SERVICE ENTRANCE DOOR WERE REPLACED. (LP# 0202940)

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 76,246 hrs · 57,890 cycles

CRACKED PREVIOUS REPAIR ON HAT CHANNEL AT FLOOR PANEL 927E. THE FLOOR PANEL WAS REPLACED IAW SRM 53-01, FIG 2.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 76,246 hrs · 57,890 cycles

CRACKED ANGLE AT BS 389 BETWEEN THE LOWER EDGE AND BEAM NR 1 ON THE FWD CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON FUEL TANK ACCESS PANEL 1367C. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A, AND SRM 51-10-3, PAR 21.

Part: FRAME — WORN (BS 1380) · airframe 76,246 hrs · 57,890 cycles

WORN FRAME TEE BS 1380, LOWER FACE BETWEEN LONGERON 24L TO 24R AT AFT ACCESORY COMPARTMENT. REPLACED THE FRAME.

Part: ACCESS PANEL — CORRODED (WING) · airframe 76,246 hrs · 57,890 cycles

CORROSION ON FUEL TANK ACCESS PLATES NBR 1371C, 1303C, 1335C. PANELS WERE REPLACED. (LP# 0201594)

Part: SPACER — CORRODED (BS 1174-1212) · airframe 76,246 hrs · 57,890 cycles

CORROSION ON SPACER AT THE AFT CARGO DOOR FRAME REPAIR, BS 1174 - 1212. REPAIRED IAW SRM 53-05, FIG 123, 51-10-3, PAR 14, 21, 38, SRM 51-30-5, AND 51-10-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON FUEL TANK ACCESS PLATES NR 1410C. FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A,

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 76,246 hrs · 57,890 cycles

DENTS ON THE UPPER & LOWER SURFACE SKIN OF THE LT ELEVATOR CONTROL TAB, AND THE ELEVATOR ANTI-FLOAT TAB. THE TAB SKIN WAS REPAIRED IAW SRM 55-04, PAR 3.

Part: ANGLE — CRACKED (BS 826) · airframe 76,246 hrs · 57,890 cycles

CRACKED ANGLE ON UPPER SURFACE BS 826, RBL 42. THE ANGLE WAS REPAIRED IAW ERA 498192-14MA, REV A.

Part: CUSP WEB — NICKED (BS 870-876) · airframe 76,246 hrs · 57,890 cycles

NICKS ON THE RT CUSP WEB BETWEEN BS 870 - 876, RBL 48 TO 52. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION OUT OF LIMITS ON RT CABIN FLOOR MEMBRANE AT STA Y =662 TO Y=667 AND Y=680 TO Y=683 IN REF NRC 00285. CUSP WEB WAS REPAIRED PER SRM 51-70-4.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

AFTER TO REMOVE CORROSION ON CUSP WEB BTW STA Y=1174 TO Y=1193, X=-54 TO X=-60, AREA WAS FOUND OUT OF LIMITS. CORROSION ON CUSP WEB BTW STA Y=1174 TO Y=1193, X=-54 TO X=-60 WAS REPAIRED PER SRM 51-70-04 FIG 2 (SHEET 1).

Part: ANGLE — CRACKED (BS 1338) · airframe 76,246 hrs · 57,890 cycles

CRACKED ANGLE AT BS 1338, LONGERON 7R AT THE AFT PRESURE BULKHEAD, THE ANGLE WAS REPAIRED IAW SRM 53-01, FIG 3.

Part: CUSP WEB — CORRODED (BS 399-401) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON THE CUSP WEB BETWEEN BS 399 - 401, RBL 44 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-4.

Part: CUSP WEB — NICKED (BS 1054-1063) · airframe 76,246 hrs · 57,890 cycles

TWO NICKS ON THE RT CABIN FLOOR CUSP WEB BETWEEN RBL 44 AND 54, BS 1054 TO 1063. THE CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 1.

Part: CUSP WEB — CORRODED (BS 598-712) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON LT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW LBL 54 AND 60 FROM BS 598 TO 712. THE CUSP WEB WAS REPLACED IAW SRM 53-05 FIG. 131A-24, AND SRM 51-30-01, 51-30-02, 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON RT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW X=-44 AND X=-60 FROM STA Y=503 TO Y=598. SECTION CUSP WEB WAS REPLACE ON STA Y= 503 TO Y=598 BTW X=-44 AND X=-60 PER SRM 53-05 FIG 131A-16, 53-05 FIG131A-24 AND SRM 51-30-01,51-30-02, 51-30-05.

Part: ANGLE — CORRODED (BS 160) · corrosion level 2 · airframe 76,246 hrs · 57,890 cycles

CORROSION ON LT LOWER EPC ANGLE BS 160 AND LBL 50. THE ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-1, AND DWG 9955780, REV LA.

Part: PIN — CORRODED (SPOILER HINGE) · airframe 76,246 hrs · 57,890 cycles

CORROSION AND WORN RT AND LT INBD FLIGHT SPOILER HINGE CENTER PINS. THE PINS WERE REPLACED.

Part: SPLICE — CORRODED (BS 503-522) · airframe 76,246 hrs · 57,890 cycles

CORROSION ON CUSP ANGLE SPLICE BETWEEN BS 503 - 522, RBL 60. THE CUSP SPLICE WAS REPLACED.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 76,246 hrs · 57,890 cycles

CRACKED ANGLE BETWEEN LOWER EDGE AND BEAM NR 1 AT AFT CARGO DOOR. THE ANGLE WAS REPLACED.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 76,246 hrs · 57,890 cycles

DELAMINATION FLOOR PANEL NR 200E, 617C, 160E AT PASSENGER CABIN. FLOOR PANEL NR 200E, 617C AND 160E WERE REMPLACED AND IDENTIFIED PER AMM 53-20-01-201.

Part: SKIN — DAMAGED (RUDDER) · airframe 76,246 hrs · 57,890 cycles

DAMAGE METALIZED COAT ON RUDDER SKIN LT AND RT SIDE. RUDDER WAS REPAIRED PER SRM 51-70-1A PAR 23 AND ERA 092613-14MA REV A.

Part: SKIN — DENTED (LT ELEVATOR TAB) · airframe 76,246 hrs · 57,890 cycles

DENTS DAMAGE ON UPPER/LOWER SURFACE SKIN AT LT ELEVATOR GEARED TAB, ALSO DEGRADED SEALANT. ELEVATOR GEARED TAB LT WAS REPAIRED PER SRM 55-04 PAR 2 C AND SRM 51-20-0.

Part: PAN — CRACKED (FUSELAGE) · airframe 76,246 hrs · 57,890 cycles

CRACK ON RING PAN UPPER FWD CORNER STA Y=846 LEFT SIDE. RING PAN UPPER FWD CORNER STA Y=846 LEFT SIDE WAS REPAIRED PER SRM 53-05 FIG 122 AND 51-10-03.

Part: TAB — DENTED (LT ELEVATOR) · airframe 76,246 hrs · 57,890 cycles

DENTS FOUND ON THE UPPER & LOWER SURFACE SKIN OF THE LT ELEVATOR CONTROL TAB, THE LT ELEVATOR ANTI-FLOAT TAB. THE LT ELEVATOR ANTI-FLOAT TAB WAS REPLACED.

Part: TAB — CORRODED (RT ELEVATOR) · airframe 76,246 hrs · 57,890 cycles

CORROSION ON LOWER SURFACE AT RT ELEVATOR CONTROL TAB, ALSO MISSING SEALANT. LEADING EDGE AT ELEVATOR ANTI FLOAT TAB. REPLACED RT ELEVATOR CONTROL TAB.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,225 hrs · 57,872 cycles

FWD FLIGHT ATTENDANT SWITCH NOT TURNING ON EMERGENCY LIGHTS. FOUND THE OVERWING EMERGENCY LIGHTS BATTERY PACK B5-49 INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-53. ALL FUNCTIONS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,923 hrs · 57,642 cycles

DURING WALK AROUND INSPECTION, FOUND DAMAGE & A HOLE IN THE BELLY SKIN. VHF ANTENNA ALSO DAMAGED AT THAT LOCATION. REPAIRED IAW PRI 559331-14, REV 0, 1, 2, 3, 4, 5, AND 6.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,915 hrs · 57,636 cycles

DURING SVC CHK FOUND EMERGENCY WING EXIT SIGNS NOT ILLUMINATING. REPLACED BATTERIES IN TWO BATTERY PACKS IAW AMM 33-53-00. OPS CHK GOOD.

Part: SKIN — CORRODED (LOWER FUSELAGE) · corrosion level 2 · airframe 75,086 hrs · 56,996 cycles

FOUND CORROSION DAMAGE ON SKIN JUST FORWARD OF THE LOWER TCAS ANTENNA.

Part: TURBINE — DAMAGED (LT ENGINE) · airframe 74,799 hrs · 56,787 cycles

ENROUTE, LEFT ENGINE EXPERIENCED COMPRESSOR STALLS AND INCREASED EGT. REDUCED POWER TO KEEP EGT IN NORMAL RANGE. FOUND TURBINE DAMAGE REQUIRING ENGINE CHANGE. ENGINE CHANGED.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 74,654 hrs · 56,663 cycles

GIRT BAR CABLE BRACKET CAME LOOSE. REINSTALLED GIRT BAR CABLE CKS OK.

Part: SLIDE — DAMAGED (TAILCONE) · airframe 73,952 hrs · 56,093 cycles

TAIL CONE SLIDE ENVELOPE APPEARS TO BE COMING UNDONE AND UNABLE TO FASTEN TO SECURE COVERING ON SLIDE. REMOVED AND REPLACED THE SLIDE IAW AMDS 5350-4644.

Part: LANYARD — FRAYED (TAILCONE) · airframe 73,952 hrs · 56,093 cycles

LANYARD FOR TAILCONE IS FRAYED. REPLACED THE LANYARD ASSY IAW AMM 53-53-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,880 hrs · 57,606 cycles

CORROSION REPAIR AT STA 208 SKIN AT GALLEY DRAIN. REPAIRED PER ERA 549712-14 SECTION 1 ON 16AUGUST16.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,880 hrs · 57,606 cycles

REPAIR OF FUSELAGE SKIN, SURROUND DOUBLER, AFT LAVATORY SERVICE DOOR CUTOUT STATION 1307, L-22L DUE TO CORROSION. REPAIR WAS ACCOMPLISHED PER ERA 549411-14 SECTION 1 ON 15AUG16.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 73,156 hrs · 55,512 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTING INOPERATIVE ON SEAT ROWS 1 THROUGH 12. A FUSE WAS FOUND BLOWN AT BATTERY PACK B5-221. THE BATTERY PACK WAS REPLACED. A WIRE WAS REPAIRED AT SEAT ROW 10D. THE EMERGENCY LIGHTS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,026 hrs · 55,407 cycles

THE CREW FOUND THAT CABIN EMERGENCY ESCAPE LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS CHECKED OK.

Part: SKIN — DAMAGED (RUDDER) · airframe 73,033 hrs · 55,414 cycles

FLAME SPRAY EXPOSED AND FLAKING ON RUDDER. RUDDER REMOVED ON AMDS CARD 2720-4187. INSTALLED RUDDER, PN 5955501-501, SN F137 IAW AMDS 2720-4421.

Part: SKIN — DAMAGED (RUDDER) · airframe 73,026 hrs · 55,407 cycles

FLAME SPRAY EXPOSED AND FLAKING ON RUDDER. RUDDER REMOVED ON AMDS CARD 2720-4187 AND INSTALLED.

Part: ANNUNCIATOR — FAILED (COCKPIT) · airframe 68,911 hrs · 52,560 cycles

DIVERTED DUE TO SMOKE IN THE COCKPIT. THE CREW REPORTED THE CAPTAIN`S FLIGHT MODE ANNUNCIATOR SMOKING AND ARCING. MAINTENANCE REPLACED THE CAPTAIN`S FMA ALL RTS WERE GOOD.

Part: PIN — WORN (TAILCONE) · airframe 68,763 hrs · 52,448 cycles

MAINTENANCE DISCOVERED THAT THE ALIGNMENT PIN FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE PIN WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: SLEEVE — DAMAGED (RELEASE CABLE) · airframe 68,763 hrs · 52,448 cycles

MAINTENANCE DISCOVERED THAT THE KEVLAR SLEEVE OVER THE RELEASE CABLE FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: SKIN — DAMAGED (BS 229-258) · airframe 68,763 hrs · 52,448 cycles

FUSELAGE SKIN AT BS 229-258, AFT OF L-1 DOOR, LONGERONS 15-17L. REPAIR DOUBLER GOUGED, DENTED, AND HAS PREVIOUS BLENDS IN AREAS. REMOVED INCOMING DAMAGED REPAIR DOUBLER & REPAIR PARTS IAW SRM 51-30-2 PG 27. NO CRACKS DETECTED ON EXISTING TRIM OUT ON SKIN. REPLACED DOUBLER & REPAIR PARTS IAW SRM 53-04-5 FIG 2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,491 hrs · 52,259 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEATS 12ABC AND 12ED WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: SEAT BELT — BINDING (F/A SEAT) · airframe 67,531 hrs · 51,624 cycles

DURING A MEDICAL EMERGENCY, THE AFT CABIN DOOR EXIT PATH WAS PARTIALLY BLOCKED BECAUSE THE AFT F/A SEAT DID NOT RETRACT FULLY. MAINTENANCE FOUND THE RT SEAT BELT RETRACTOR RUBBING AND REPOSITIONED THE BELT CORRECTLY. OPERATION THEN CHECKED NORMALLY AND THE SEAT FULLY RETRACTED.

Part: DUCT — BLOWN (ACM) · airframe 67,141 hrs · 51,356 cycles

F/A REPORTED AN ELECTRICAL SMOKE ODOR EMANATING FROM BOTH OF AFT LAVATORIES. FLIGHT CREW SECURED CIRCUIT BREAKERS FOR LAVATORY LIGHTING, LAVATORY FLUSH MOTORS, AND LAVATORY WATER HEATERS. ODOR DISSIPATED, MAINTENANCE FOUND A BLOWN DUCT FOR RT SIDE AIR CYCLE MACHINE. FLEXIBLE DUCT RECONNECTED AND HANGER SUPPORT CLAMP FOR IT WAS SECURED. ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,072 hrs · 51,301 cycles

DURING LINE CHECK IN TPA, THE CABIN OVERHEAD EMERGENCY EXIT LIGHTS ON RT SIDE WERE FOUND TO BE INOPERATIVE FROM ROWS 16 THRU 36. REPLACED BATTERIES IN POWER SUPPLIES IAW AMM 33-53 AND OPERATION IS NOW NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 67,057 hrs · 51,292 cycles

SEAT 16 AND 17 EMERGENCY LIGHTS DAMAGED. REPLACED EMERGENCY PATH LIGHT ASSY AT ROW 16 AND 17 IAW CHAPTER 20. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,978 hrs · 50,555 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT THE COCKPIT DOOR AND AT DOORS L1 & L2 WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: ACM — OVERTEMP (RIGHT) · airframe 65,603 hrs · 50,292 cycles

FLIGHT DIVERTED, AFTER THE CABIN CREW REPORTED AN INTERMITTENT BURNING ODOR. MX COULD NOT FIND ANY POSITIVE SOURCE FOR THE ODOR. THE RT ACM WAS REPLACED DUE TO SUSPECTED OVERTEMP. A DUCT BURNOUT WAS ACCOMPLISHED AND THE ACFT HAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 65,562 hrs · 50,262 cycles

DURING MX, A WIRE WAS FOUND BROKEN SUPPLYING POWER TO THE LT VENTRAL STAIR EMERGENCY EXIT LIGHT. THE EMERGENCY LIGHT WIRING WAS REPAIRED IAW WIRING MANUAL REF 20-50.

Part: SKIN PANEL — DAMAGED (HORIZ STAB) · airframe 64,929 hrs · 49,809 cycles

HORIZ STAB UPPER CENTER SKIN PANEL REPAIRED IAW 09-484168-12.

Part: LIGHT — ODOR (CABIN) · airframe 62,377 hrs · 48,042 cycles

WHILE IN CRUISE AT FL350, THE FLIGHT ATTENDANT REPORTED A "BURNING SMELL" NEAR SEAT ROW 27. THE UPPER & LOWER SIDEWALL CABIN LIGHTS WERE TURNED-OFF AND THE GALLEY POWER WAS SECURED. FURTHER REPORTS WERE THAT THE SMELL HAD DISSIPATED BY DESCENT TIME. LANDING AT BUF WAS UNEVENTFUL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,135 hrs · 47,882 cycles

A/C INCURRED GROUND DAMAGE ON THE FUSELAGE SKIN AND STRUCURE BELOW THE L1 DOOR AND BELOW THE FWD AIRSTAIR DOOR. REPAIRS C/W ON ERA 496866-14.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 62,135 hrs · 47,882 cycles

DAMAGED SHEAR TIE AT FS 180 AT STR 23L. REPAIRED PER ERA 496962-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV TOOLING MARKS WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=1022-1041 BETWEEN LONGERON 30 TO 27RT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=196.25 BETWEEN LONGERON 20LT AND 21LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-05 FIG 57A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV THREE CRACKS WERE FOUND OF .125",.093" AND .062" ON FUSELAGE SKIN AT STA Y=737.5,374 AND 375.5 BETWEEN LONGERON 20 AND 21RT AT THE DOORJAMB UPPER CORNER FWD CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW ERA 494036-14 REV ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=1022-1041 BETWEEN LONGERON 27LT TO 28LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=1117-1122 BETWEEN LONGERON 27 AND 26LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=769-788 BETWEEN LONGERON 28RT TO 28LT AT MID CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN PANEL — DELAMINATED (SPOILER) · airframe 61,681 hrs · 47,546 cycles

DURING HMV DELAMINATION WAS FOUND ON RT GROUND SPOILER PANEL AND WEAR ON LOWER SURFACE. SPOILER PANEL UPPER SURFACE WAS REPAIRED IAW SRM 51-70-1B PARA 8 AND LOWER SURFACE REPAIRED IAW SRM 51-10-3B.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLER FROM STA Y=750 TO 759.5 BETWEEN LONGERON 26LT AND 26RT. DOUBLER WAS REPLACED IAW DOUGLAS DRAWING 5936004-7 REV AN.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN STA Y=1060 TO Y=1066 X=6 TO X=-6. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV TRANSFERED FROM ADF DENT 4 INCHES ABOVE FWD CARGO DOOR CUTOUT FWD CORNER. DUE TO DENT WAS FOUND CLOSE TO DAMAGE REPORTED OF CRACKS ON FWD CARGO DOOR FWD UPPER CORNER SKIN WAS REPAIRED IAW ERA 494036-14 REV ORIG REF NRC T0212163.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN FROM STA Y=763 TO 826 BETWEEN LONGERON 27RT AND 30. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN AT STA Y=788, 807 BETWEEN LONGERON 28LT AND 30 AND Y=864 TO 905 ON LONGERON 18LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: STRUCTURE — ERODED (RUDDER) · airframe 61,681 hrs · 47,546 cycles

DURING HMV DAMAGED METALIZED COAT WAS FOUND ON LT AND RT FACE OF RUDDER. RUDDER WAS REPAIRED IAW SRM 51-70-1A PARA 23.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=1130-1136 BETWEEN LONGERON 29RT TO 29LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: TAB — DAMAGED (RUDDER) · airframe 61,681 hrs · 47,546 cycles

DURING HMV DAMAGED METALIZED COAT WAS FOUND ON RUDDER CONTROL TAB. RUDDER TAB WAS REPAIRED IAW SRM 51-70-1AD PARA 23.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN FROM STA Y=840, 947 TO 1003 LONGERON 18RH,Y=1073 BETWEEN LONGERON 18RT AND 19RT,Y=1079 TO 1136 BETWEEN LONGERON 26RT AND 30. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION ON INNER FUSELAGE SKIN BETWEEN STA Y=1060-1076 BETWEEN LONGERON 27LT TO 29LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=1119 BETWEEN LONGERON 27LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: BEAM — CRACKED (R1 DOOR) · airframe 61,681 hrs · 47,546 cycles

CRACKED BEAM NR 1 ON FWD STRUCTURE ALSO CRACKED BEAM NR 4 CRACKED ON R1 DOOR. REPAIR ANGLE INSTALLED IAW MD88 SRM 52-05 FIG 25 ITEM 15.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN FROM STA Y=1079 TO 1136 BETWEEN LONGERON 24LT AND 30. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — NICKED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV A NICK WAS FOUND ON FUSELAGE SKIN STA Y=200 BETWEEN LONGERON 20LT TO 21LT. FUSELAGE SKIN WAS REPAIRED IAW ERA 494043-14 REV ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=788-807 BETWEEN LONGERON 29LT TO 29RT AT MID CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=1079-1098 BETWEEN LONGERON 28LT TO 30 AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DUE TO FUSELAGE SKIN REPAIR PREVIOUS REPAIR FOUND ON INTERNAL DOUBLER BETWEEN STA Y=617 TO 636 AND LONGERON 29LT TO 29RT WILL NEED TO BE REPLACED. PREVIOUS REPAIR WAS REPLACED IAW ERA 494058-14 REV ORIG REF NRC T0212237.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN BETWEEN STA Y=1098-1104 BETWEEN LONGERON 29LT TO 29RT AT AFT CARGO COMPARTMENT. FUSELAGE WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: BEAM — CRACKED (R1 DOOR) · airframe 61,681 hrs · 47,546 cycles

CRACKED BEAM NR 1 AND NR 4 FWD SECTION OF R1 DOOR. INSTALLED REPAIR ANGLE IAW MD88 SRM 52-05 FIG 24 ITEM 15.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

CORROSION ON LOWER FUSELAGE SKIN STA Y=726 LONG 29RT. SKIN SECTION SPLICE REPAIR WAS ACCOMPLISHED IAW ERA 494046-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

ELONGATED HOLES FUSE SKIN BETWEEN L1 AND L2 STA 1414 AND 1422 ALSO PLUGGED SKIN STA 1415. ELONGATED HOLES AND PLUGGED SKIN REPAIRED IAW ERA 494060-14 REV ORIG.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

TOOL MARKS ON P-DOME T AT STA 1338 AND PROJECTION OF LONG 25RT. NEW SECTION OF LOWER T WERE INSTALLED IAW ERA 49457 4-14 REV ORIG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

CORROSION ON DOOR JAMB LOWER BEAM OF MID CARGO COMPARTMENT BETWEEN STA Y=636-693 AT C2 COMPARTMENT. REPAIR ACCOMPLISHED IAW MD88 SRM 53-05 FIG 123.

Part: SKIN — BROKEN (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

BROKEN FUSE SKIN STA 1421 BETWEEN L1R AND L2R. FUSE SKIN REPAIRED IAW ERA 494060-14 REV ORIG.

Part: SKIN — BROKEN (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

BROKEN FUSELAGE SKIN STA 1418 BETWEEN L1-L2 LT. SKIN REPAIR ACCOMPLISHED IAW ERA 494060-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

TOOL MARKS ON LT WINDOW CUTOUT NR 67 AND AFT LWR CORNER WINDOW NR 5. BLENDED AREA IAW ERA 494034-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

LIGHTNING STRIKES ON UPPER SECTION OF LT CABIN WINDOW NR 55 AND FWD CENTER SECTION OF CABIN WINDOW NR 59. BLENDED AREA IAW ERA494035-14 REV ATIME LIMITED REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

LIGHTNING STRIKES AFT CNTR SECTION CABIN WINDOW CUTOUT NR 51 AND NR 53. BLENDED AREAS IAW ERA 494035-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

LIGHTNING STRIKES ON LWR AFT CORNER OF LT CABIN WINDOW CUTOUT NR 35 AND LWR FWD CORNER CABIN WINDOW CUTOUT NR 37. BLENDED AREAS FOR TIME LIMITED REPAIR IAW ERA 494035-14 REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

LIGHTNING STRIKES ON LT CABIN WINDOW NR 33 CUTOUT. BLENDED AREA IAW ERA 494035-14 REV A.

Part: BEAM — CRACKED (R1 DOOR) · airframe 61,681 hrs · 47,546 cycles

CRACKED BEAM NR 1 ON FWD SECTION ALSO CRACKED BEAM 4 ON FWD SECTION OF R1 DOOR STR. REPAIR DOUBLERS INSTALLED IAW MD88 SRM 52-05D FIG 25.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 61,681 hrs · 47,546 cycles

CORROSION ON BARREL NUT HOLE NR 14 RT UPPER HORIZ STAB. CORROSION REMOVED AND BUSHING INSTALL IAW EA 494039-14 REV ORIG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,681 hrs · 47,546 cycles

CRACKED INNER AND OUTER PAN BEHIND STOP NR 5 AT FWD CARGO DOOR AFT SECTION. STOPPED DRILLED AND INSTALLED DOUBLER REPAIR IAW MD88 SRM 52-03 FIG 8.

Part: BELT — DAMAGED (FUSELAGE) · airframe 61,681 hrs · 47,546 cycles

LIGHTEING STRIKE ON RT WINDOW BELT FRAMES BETWEEN STA Y=256-237, 275-256, 294-275, 313, 294, 332-313, 351-332 AND 465-446. BLENDED AREAS IAW ERA 494034-14 REV A. CONTINUE SERVICE AS-IS.

Part: SHEAR TIE — CORRODED (BS 1309 L21) · airframe 60,951 hrs · 47,033 cycles

PCK-N CORROSION ON SHEAR TIE AFT CARGO AT STA 1309 LONGERON 21. ACCOMPLISHED PERMANENT REPAIR PER ERA 490408-14 REV ORIGINAL.

Part: DOUBLER — CORRODED (BS 212 L29-30R) · airframe 60,951 hrs · 47,033 cycles

PSV VISIT, CORROSION ON JACK PAD FITTING INTERIOR DOUBLER STA 212 BETWEEN L-29R AND L-30. REMOVED EXISTING DOUBLER AND FABRICATED NEW DOUBLER 9911520-147 FROM 7075-T6 .063 INCH IAW DWG 9951888. INSTALLED DOUBLER PER DOUGLAS DRAWING 9951888. RII COMPLETE. INSTALLED FLOOR PANEL.

Part: LIGHT — INOPERATIVE (SEAT 17D) · airframe 60,729 hrs · 46,900 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATH LIGHT AT 17D INOPERATIVE. MX REPLACED LIGHT ASSY IAW AMM33-53-01. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: LANYARD — MISINSTALLED (L2 DOOR SLIDE) · airframe 60,729 hrs · 46,900 cycles

DURING LINE CHECK, MX FOUND L2 DOOR SLIDE LANYARD INSTALLED INCORRECTLY. MX REPOSITIONED DOOR SLIDE LANYARD IAW AMM 25-62-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,015 hrs · 46,426 cycles

FOUND ON ARRIVAL - DENT AND SCRAPE APPROX 2 FT AFT OF L-1 DOOR (FS 229). REPAIRED ON N/R CARDS 1 AND 3 PER ERA 486506-14 REV ORIG. (DLM88102779).

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,940 hrs · 46,372 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT ROW 1-4 AND 10-12 INOPERATIVE. MX REPLACED POWER SUPPLY IAW M/M. REINSTALLED ORIGINAL BATTERY PACK IN NEW POWER SUPPLY. OPERATION OF LIGHTS NOW CHECKS OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 59,800 hrs · 46,263 cycles

DURING LINE CHECK, MX FOUND FIRST CLASS LAVATORY EMERGENCY FLOOR LIGHTS INOPERATIVE. MX SECURED CONNECTOR. OPS OF LIGHT NOW CHECKS OK.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 59,219 hrs · 45,846 cycles

VERTICAL STABILIZER, L/E SKIN, UPPER REMOVABLE PANEL, LOWER EDGE WEAR DAMAGE REPAIRED IAW ERA 483216-14.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 59,218 hrs · 45,845 cycles

VERT STAB REMOVABLE L/E UPPER EDGE HOLES DAMAGED, REPAIRED IAW ERA 483240-14.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 58,943 hrs · 45,649 cycles

THE EMERGENCY LIGHT AT SEAT 3C WAS FOUND TO BE INOPERATIVE. FOUND PIN PULLED OUT OF SPLICE UNDER SEAT 3C. SECURED PIN. OPS CHKS GOOD.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 57,464 hrs · 44,690 cycles

FUSELAGE AFT PRESSURE DOME LOWER CHORD REPAIRED IAW EA 09-086680-12, ME15.

Part: OIL SYSTEM — LEAKING (APU) · airframe 56,257 hrs · 43,887 cycles

LIGHT HAZE AND ODOR IN CABIN, APU OIL LEAK, DEFERRED APU, OPN 5089 DUCT BURN-OUT. REMOVED APU DOOR ASSEMBLY CLEANED ASSEMBLY AND APU AND UPPER SIDE OF AIR BOX. REPLACED ALL REMOVED RAN APU AND CHECKED FOR ODOR AND SMOKE. ALL OPS NORMAL NO DEFECTS. MCO AND PLACARD REMOVED.

Part: LATCH — UNKNOWN (COWLING) · airframe 54,397 hrs · 42,707 cycles

ENGINE UPPER COWL DOOR LATCH REPLACED IAW EA 09-056907-12, ME05.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 53,756 hrs · 42,286 cycles

POSSIBLE COMPRESSOR STALL LT ENGINE ON TAKEOFF ROLL, REJECTED TAKEOFF ROLL AT 75 KTS. MTC IN PROGRESS REPLACING LT ENGINE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,925 hrs · 41,771 cycles

FUSELAGE SKIN FOUND WITH CORROSION AT STA 620 BETWEEN L-29L AND L-29R. CUTOUT DAMAGED SKIN AND INSTALLED A DOUBLER.

Part: TRANSFORMER — BURNED (CABIN) · airframe 52,716 hrs · 41,654 cycles

SMOKE AND FUMES IN CABIN. FOUND VARIABLE TRANSFORMER FOR LOWER SIDE WALL PANEL BAD AT AFT F/A PANEL. REMOVED AND REPLACED ON ITEM 5 TRANSFORMER HAD STRONG BURNED ELECTRICAL ODOR PERFORMED ALT DUCT BURN ON ITEM 7.

Part: SUPPORT BEAM — PUNCTURED (NLG) · airframe 50,418 hrs · 40,216 cycles

NLG SUPPORT BEAM, RT FS 94 WEB PUNCTURE REPAIRED IAW ERA 459315-14.

Part: SKIN — CORRODED (BS 750 L30) · airframe 48,557 hrs · 38,970 cycles

THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 750, L-30. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: WATER HEATER — OVERHEATED (AFT LEFT LAV) · airframe 45,936 hrs · 37,113 cycles

AFT LEFT LAV HAD SMOKE / ELECT BURNING SMELL EMITTING FROM IT. REPLACED OVERHEATED WATER HEATER AND CONNECTOR.

Part: BALLAST — FAULTY (CABIN) · airframe 43,992 hrs · 35,686 cycles

WISPY SMOKE REPORTED OVER SEAT 25DE. REPLACED BALLAST, CHECKS GOOD.

Part: DUCT — BLOWN (#2 ENGINE) · airframe 38,903 hrs · 32,126 cycles

RT ENG THROTTLE AND FUEL LEVER BINDING WORK IN PROGRESS. PLEASE UPDATE. CA FND A/I DUCT BLOWN. REPLD.ANTI-ICE VLV PRESSURE SWITCH.BAND DUCT. LEAK CKS GOOD.

Part: SEAL — BROKEN (APU) · airframe 38,353 hrs · 31,716 cycles

SMOKE DETECTOR ACTIVATED IN LAV F/O SIDE ON T/O TO 8000 FT, THEN WHEN OUT, NO ENG / WING ICE ON CROSS FEEDS CLOSED. FOUND APU OIL CAP SEAL BROKEN. REPLACED APU OIL CAP. REMOVED APU INLET PANEL AND CLEANED. PERFORMED STEPS 1-7 OF DUCT BURN OUT. COMPLIED WITH DUCT BURN OUT OP 5088.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 36,868 hrs · 30,616 cycles

AFTER TAKEOFF PASSING 3K FEET THE AFT RIGHT LAV SMOKE DETECTOR ACTIVATED. NO OTHER SIGN OF SMOKE OR FIRE DETECTED FROM CABIN CREW. CKD APU INLET, NTF. BOROSCOPED NR 1 ENGINE, FOUND EVIDENCE OF OIL LEAKING NR 3 SEAL AREA. REPLACED NR 1 ENGINE PER ROUTINE CARD DECK TRANS.

Part: INLET — CONTAMINATED (APU BAY) · airframe 36,789 hrs · 30,555 cycles

AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN WITH MULTIPLE LEVEL SMOKE DETECTORS GOING OFF. IMMEDIATE LANDING AT JFK. FOUND OIL IN APU COMPT AND APU INLET AREA. CLEANED INLET, PERFORMED DUCT BURNOUT.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 36,244 hrs · 30,143 cycles

FLIGHT ATTENDANT REPORTED BURNING SMELL IN ENTIRE CABIN DURING T/O. THE SMELL DISSIPATED DURING CLIMBOUT AND WAS GONE AROUND 10000 FEET. CHANGED WATER SEPERATOR BAGS PERFORMED DUCT BURN OUT PER M/M . RAN ENGINES AT ALL POWER SETTINGS NO SMELL NOTED CKS GOOD A/C OK FOR SVC

Part: PIN — UNSERVICEABLE (ESCAPE SLIDE) · airframe 34,262 hrs · 28,683 cycles

PINS PULLED OUT OF 1R SLIDE COVER. REPLACED SLIDE.

Part: TURBINE — FAILED (NR 2 ENGINE) · airframe 33,588 hrs · 28,180 cycles

AFTER ROTATION, RIGHT ENGINE STALLED AND LOST POWER, EGT WENT TO 800 DEGREES. SHUTDOWN ENGINE AND RETURNED TO ORD. TURBINE FAILED. REPLACED ENGINE.

Part: SKIN — DENT (BS 229 - 245)

THE FUSELAGE SKIN WAS FOUND DENTED AT FROM FS 229 TO 245 BETWEEN L16L AND L18L. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333836-14.

Part: LIGHT — BROKEN (R1 DOOR)

LENS OF R1 DOOR EMERGENCY BROKEN. REPLACED LIGHT ASSY. OPS CKS NML.

Part: COALESCER BAG — DIRTY (CABIN)

NOTED MUSTY ODOR IN CABIN SHORTLY AFTER T/O AT 1000 AGL. F/A REPORTED SMOKE IN CABIN, RETURNED TO CVG. A/I NOT IN USE, OVEN AND SIDEWALL LIGHTS OFF, APU AIR ON PREVIOUS MCO. CHANGED WATER BAGS AND PERFORMED DUCT BURNOUT, ALL CKS OK.

Part: LINE — WORN (RT PYLON)

RIGHT HYD SYSTEM PRESSURE INDICATES ZERO AND HYD QUANTITY SHOWS 3 QTS. FOUND PRESSURE LINE AT RT ENG PYLON WORN THRU BY CLAMP. REPLACED HOSE AND CLAMP. ALSO, CASE DRAIN FILTERS, NO METAL FOUND. SERVICED HYD, RAN ENG AND AUX PUMP, NO LEAKS FOUND.

Part: FUEL CONTROL — FAILED (NR 1 ENGINE)

AFTER T/O, F/A SMELLED BURNING RUBBER IN AFT CABIN, AT 18000 LOST POWER ON NR 1 ENG. FLT RETURNED TO ATL WITH NR 1 ENG AT IDLE. REPLACED NR 1 ENGINE FUEL CONTROL. UNABLE TO DUPLICATE SMELL.

Part: HYD LINE — PUNCTURED (N2 ENGINE)

RT HYD SYSTEM FAILURE CLIMBING OUT OF TYS. REPLACED RT ENG HYDRAULIC PRESSURE LINE AT FIREWALL AND MAIN GEAR DOOR SKID PADS, ALL LK CHECKS OK.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVS)

AT TOP OF DESCENT FL330, F/A REPORTS BOTH AFT SMOKE DETECTORS GOING OFF. F/O CKD FOR SMOKE/HT, NONE NOTED. AFTER REACHING CRZ- SMOKE DETECTORS SHUT OFF. CHECKED INLET AND EXHAUST ON BOTH ENGINES. CHECKED LEFT AND RIGHT ACMS. STEAMED CLEANED APU INLET, ALL CHECKED GOOD. NOTHING FOUND, REPLACED WATER SEPARATOR BAGS AS PRECAUTIONARY. RAN ENGINES NOTHING FOUND.

Part: OVEN — DIRTY (GALLEY)

UPON LEVELING AT FL 330, SMELLED SMOKE, SIMILAR TO FOOD BURNING IN OVEN. OVENS HAD BEEN TURNED ON DURING CLIMB-OUT. FWD AND AFT LAV SMOKE ALARMS WENT OFF. TURNED OVENS OFF AND SMOKE DISSAPATED, ALARMS SILENCED. REPOSITIONED LOOSE SEAL ON AFT GALLEY OVEN DOOR AND REMOVED SOILED FOOD CARRIER FROM SAME OVEN.

Part: SPRAY DEFLECTOR — BROKEN (NLG)

ON T/O, COULD NOT RAISE THE NOSE GEAR HAD A RED LIGHT UNSAFE ON NOSE GEAR ONLY. FOUND LEFT HAND NOSE SPRAY DEFLECTOR BROKEN. REPLACED SAME, RAN NOSE GEAR, CHECKS GOOD.