N935DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,730 hrs · 56,497 cycles

EMERGENCY CEILING LIGHTS AT SEATS 16-19 INOPERATIVE. REPLACED THE BATTERIES AT B5-102. CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,791 hrs · 55,733 cycles

FWD GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-50. OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 942) · airframe 73,033 hrs · 55,164 cycles

FOUND A CRACK ON THE FRAME WEB, FWD SIDE. LOCATED 4 FASTENERS BELOW LONGERON 7L, BS 942.225. REPAIRED IAW SRM 53-03D FIG. 38D.

Part: BRACKET — BROKEN (BS 942) · airframe 73,035 hrs · 55,166 cycles

FOUND BROKEN BRACKET ON RT CANTED FRAME, AFT SIDE. LOCATED AT THE OTBD END OF STIFFENER LONGERON 7R, BS 942.225. REPLACED THE BRACKET.

Part: ANGLE — CRACKED (BS 942) · airframe 73,035 hrs · 55,166 cycles

FOUND LOWER ANGLE CRACKED AT BS 942.225 ON LOUVER FWD FRAME. REPLACED THE ANGLE.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 72,725 hrs · 54,945 cycles

L1 DOOR SLIDE PINS PULLED. REPLACED L1 DOOR SLIDE IAW JIC 2561-4964, OK FOR SERVICE.

Part: BLOCK — DAMAGED (RELEASE CABLE) · airframe 70,876 hrs · 53,547 cycles

TAIL INTERIOR, TAIL CONE RELEASE LOCK CABLE BLOCK IS NOT .5" AWAY FROM TUBING, CONDUIT, AS REQUIRED IAW STEP 7. OPS CHECKED GOOD IAW AMDS 5350-01077-0101.

Part: THRESHOLD — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

FOUND ON "OK TO TREAT", L1 DOOR, THRESHOLD, INBD THRESHOLD/FLOORBOARD SUPPORT, 4" FROM DOOR OPENING, CORRODED, IN MULTIPLE AREAS ALONG ENTIRE LENGTH OF SUPPORT. TREATED PRIMED AND PAINTED AND INSTALLED IAW DWG 9936534.

Part: SCUFF PLATE — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

MID CARGO BAY DOOR LOWER JAMB UNDER ENTERY SCUFF PLATE CORRODED. REPAIRED IAW ER/A 499523-14MA, REV O.

Part: FINGER DOUBLER — CORRODED (BS 1287-1300) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, LAP SEAM FINGER DOUBLER HAS CORROSION, NEAR L26L, BS 1287-1300. REPAIRED IAW SRM 53-01, FIG 1.

Part: LONGERON — CORRODED (BS 1295) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, LONGERON 26L SPLICE CORRODED BLOW OUT, BS 1295. INSTALLED LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18 CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.

Part: FRAME — CORRODED (BS 1309) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, FRAME AT BS 1309 AFT SIDE HAS CORROSION ABV L27-26L. REPAIRED IAW SRM 53-01, FIG 1 FOUND CORROSION TO BE LEVEL 1.

Part: FRAME — CORRODED (BS 1287) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, B-FRAME AT BS 1287 AFT FACE HAS CORROSION, OTBD OF L25L. REPAIRED IAW SRM 53-01, FIG 1.

Part: LONGERON — CORRODED (BS 1322) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

LONGERON 23 LT HAS CORROSION, BS 1322, INSTALLED. LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18, CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.

Part: LONGERON — CORRODED (BS 1295) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, LONGERON 25L, SPLICE HAS CORROSION AT BS 1295. COMPLETED LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18 CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.

Part: LONGERON — CORRODED (BS 1290-1300) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, L29L HAS CORROSION, BS 1290-1300. REPAIRED IAW SRM 53-01, FIG 1.

Part: SHEAR TIE — CORRODED (BS 1193) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO COMPARTMENT, LAV SPILL: SHEAR TIE CORRODED BS 1193 BETWEEN L29L TO L30. MAX MATERIAL REMOVED WAS .005" FROM ORIGINAL THICKNESS OF .071" IAW DWG 9936073. PART IS WITHIN LIMITS IAW SRM 53-01, FIG 1.

Part: SHEAR TIE — CORRODED (BS 1287) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, SHEAR TIE AT BS 1287 AFT SIDE HAS CORROSION, L29L TO L26L. REPAIRED IAW SRM 53-01, FIG 1.

Part: DOOR SILL — CORRODED (BS 1212) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

AFT CARGO COMPARTMENT AFT DOOR SILL SUPPORT GUSSET HAS CORROSION, BS 1212. REPLACED SUPPORT.

Part: LONGERON — CORRODED (BS 1287-1322) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, L27L HAS MANY SPOTS OF CORROSION, BS 1287-1322. REPAIRED IAW SRM 53-01, FIG 1.

Part: LONGERON — CORRODED (BS 1289) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

LONGERON 23L AT BS 1289 CORRODED. REPLACED SPLICE AND LONGERON IAW SRM 53-02, FIG 18, CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.

Part: LONGERON SPLICE — CORRODED (BS 1300) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, L22L SPLICE AT BS 1300 HAS CORROSION. REPAIRED IAW SRM 53-01 FIG 1.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL-L25L HAS CORROSION, BS 1287-1309. INSTALLED LONGERON AND SPLICE REPAIR IAW 53-02, FIG 18 CORROSION FOUND TO BE LEVEL 2 CAUSED BY A LAV SPILL.

Part: LONGERON — CORRODED (BS 1287-1309) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, L29R HAS CORROSION, BS 1287-1309. REPAIRED IAW SRM 53-01, FIG 1.

Part: LONGERON — CORRODED (BS 1290) · airframe 70,876 hrs · 53,547 cycles

L22 AT ST 1290 CORRODED. REPAIRED IAW SRM 53-01, FIG 1.

Part: LONGERON — CORRODED (BS 1290) · airframe 70,876 hrs · 53,547 cycles

AFT CARGO BILGE, LAV SPILL, L24L HAS CORROSION BLOW OUT AT BS 1290. REPAIRED IAW SRM 53-01, FIG 1.

Part: FRAME — CORRODED (BS 1322) · airframe 70,876 hrs · 53,547 cycles

FRAME AT ST 1322 AT LT L23 CORRODED. REPAIRED IAW SRM 53-01, FIG 1.

Part: BUTT JOINT — CORRODED (BS 1174-1193) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

AFT CARGO COMPARTMENT, LAV SPILL, BUTT SPLICE CORRODED AND STAINED BETWEEN BS 1174 AND 1193, L26L TO L28R. REPAIRED IAW SRM 53-01, FIG 1.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

MID CARGO COMPARTMENT SHIM SPACER UNDER FWD LOWER JAMB DOOR STOP CORRODED, EXFOLIATED, FASTENERS HEADS GOING THROUGH LOWER SKIN THROUGH DOOR STOP ARE POPPED. REPAIRED IAW 53-05, FIG 123A.

Part: FLOOR SUPPORT — CORRODED (BS 786) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

MID CARGO COMPARTMENT HAS CORROSION UNDER FLOOR SUPPORT NUTPLATES BS 786. REPLACED FLOOR SUPPORT SRM 51-30-02.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 70,876 hrs · 53,547 cycles

MID CARGO COMPARTMRNT, SHIM, SPACER UNDER FWD LOWER JAMB DOOR STOP CORRODED, EXFOLIATED, FASTENERS HEADS GOING THROUGH LOWER SKIN THROUGH DOOR STOP ARE POPPED. REPAIRED IAW 53-05, FIG 123A.

Part: SKIN — CRACKED · airframe 69,984 hrs · 52,937 cycles

FOUND APPROXIMATELY 1.75 CRACK IN SKIN APPROXIMATELY 6 IN AFT FROM ELEVATOR ACCUMULATOR ACCESS DOOR. ELEVATOR ACCUMULATOR ACCESS DOOR CUTOUT SKIN CRACKED FROM UPPER AFT CORNER RADIUS TO CLOSEST FASTENER AFT. C/W PRI 542690-14, REV 0,1,2,3,4 AND FINAL, C/W ERA 542690-14, REV ORIGINAL NO CHANGES NOTED. PERMANENT REPAIR.

Part: SKIN — DAMAGED · airframe 69,984 hrs · 52,937 cycles

THREE LIGHTINING STRIKE DAMAGE LOWER FORWARD FUSELAGE JUST AFT OF ELECTRONIC EQUIPMENT COMPARTMENT ACCESS. 1, 7" AFT OF ELECTRONIC EQUIPMENT CUTOUT AT S29R, 2, 9.5 " AFT OF E/E CUTOUT 3" RT OF S30 AT FASTENER. 3, 11" AFT OF ELECTRONIC EQUIPMENT CUTOUT 3" RT OF S30. DRILLED OUT DAMAGE AT NR 1 LOCATION IAW SRM 53-04-02, PAGE 9, 2A. NEEDS PLUG AND PAINT AND NDT. LOC 2, BLENDED DAMAGE LESS THAN .010" SRM 51-02, STEP 3, PAGE 3, NEEDS PAINT. LOC 3 BLENDED DAMAGE LESS THAN .010 SRM 5-02, STEP 7, PAGE 3, NEEDS PAINT. RESTORED FINISH AT LOC 2 AND 3 IAW PS 900-3. LOCATION 1 AND 2 NO ITEMS INSTALLED PERMANENT PLUG REPAIR, REF IAW 542702, REV 1. RESTORED FINISH IAW PS 900-3. REPAIR FOR ITEM 1 C/W IAW ERA54442702-14, REV ORIG FILE CODE 0053-30, DATED 31, DEC 2015 TIME LIMITED TO 12 MONTHS.

Part: HOUSING — WORN (RELEASE CABLE) · airframe 69,266 hrs · 52,428 cycles

MAINTENACE FOUND AFT ENTRANCE DOOR TAILCONE RELEASE PULL CABLE HOUSING WORN. THE TAIL CONE RELEASE CABLE WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,030 hrs · 52,245 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 11-15 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,001 hrs · 52,223 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 11-14 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 68,915 hrs · 52,172 cycles

DURING CLIMBOUT AT ABOUT FL200, RT MAIN GEAR RED LIGHT ILLUMINATED. SEVERAL MINUTES LATER AMBER GEAR DOOR OPEN LIGHT ILLUMINATED INTERMITTENTLY. AT FL250 LEVELED OFF AND LIGHT CONTINUED. RAN QRH 14.19, THRU STEP 3. AUTO SPEEDBRAKE RESET ON ITS OWN. ALL LIGHTS EXT OPS NORMAL, SPEED 310K, SLOWED TO 230. JACKED ACFT & PERFORMED PSEU BITE CHECK WITH GEAR UP & DOWN, NO FAULTS NOTED. PERFORMED TSM 32-60-00 PG BLK 101, NO FAULTS NOTED, IAW MCC, R & R RT MLG RETRACT ACTUATOR IAW AMM 32-32. OK FOR SERVICE. CYLINDER, MLG RT OFF 88-3231-9-0001-00004 ON 88-3231-9-0001-01540.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 68,365 hrs · 51,796 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT SEAT 14D. MAINTENANCE CONNECTED A DISCONNECTED CONNECTOR AND THE OPS CHECKED GOOD.

Part: STRIKER — OUT OF POSITION (TAILCONE RELEASE) · airframe 65,571 hrs · 49,792 cycles

PERFORMED TAILCONE RELEASE SYSTEM OPS CHECK, SYS FAILED, AND MAINTENANCE FOUND THE TAILCONE EXTERIOR RELEASE CABLE PULL FORCE WAS OUT OF ALLOWABLE LIMITS. FOUND WAS THE DOOR JAMB UPPER FITTING WAS OUT OF CONFIGURATION AND WAS CORRECTED BY REMOVING THE STRIKER PLATE. THE SYS WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.

Part: PULLEY — WORN (TAILCON RELEASE) · airframe 65,563 hrs · 49,789 cycles

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

Part: BRACKET — WORN (CABLE CAM) · airframe 65,563 hrs · 49,789 cycles

MAINTENANCE DISCOVERED THAT THE KEVLAR CABLE CAM BASE BRACKET FOR THE TAILCONE WAS WORN, OUT OF ALLOWABLE LIMITS. THE KEVLAR CABLE CAM BASE BRACKET WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 64,812 hrs · 49,280 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 12DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: AIRSTAIR — LACK OF LUBE (TAIL) · airframe 62,912 hrs · 47,888 cycles

CATWALK IN TAIL SECTION DOWN, WILL NOT COME UP WITH AIRSTAIRS DOWN. FOUND NO DAMAGE TO LIFT CABLES OR RIGGING. SPRINGS DO NOT APPEAR TO BE BROKEN BUT MAY BE WORN OUT. VERIFIED DOWNLOCK PIN OPERATES NORMALLY. LUBED CATWALK OPS CHECKS GOOD IAW AMM 52-62.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,283 hrs · 47,442 cycles

FUSELAGE FRAME CRACKED AT LONGERON 1. REPAIRED IAW ER/A 489679-14 REV C. CHECKED GOOD.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 62,259 hrs · 47,425 cycles

DENTS, SCRATCHES, GOUGES, AND CRACKS ON INNER AND OUTER SURFACE OF AFT CARGO COMPARTMENT DOOR BARRIER. AFT CARGO COMPARTMENT DOOR BARRIER WAS REPAIRED IAW ER/A 094625-14 MA REV C ASSOCIATED ER/A 09-462514.

Part: SUPPORT — DAMAGED (BS 655) · airframe 62,259 hrs · 47,425 cycles

CRACK ON UPPER CHANNEL SUPPORT BS 655 OF MID CARGO COMPARTMENT DOOR BARRIER. DAMAGE WAS REMOVED DOUBLER WAS FABRICATED WAS INSTALLED IAW ER/A 383099-14MA, REV ORIG.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 62,259 hrs · 47,425 cycles

HORIZONTAL STAB UPPER LT FAIRING YH 85, CRACKED. PERMANENT REPAIR WAS ACCOMPLISHED IAW ER/A 464594-14 REV B REPAIR

Part: ANGLE — DAMAGED (RT WING) · airframe 62,259 hrs · 47,425 cycles

CRACK 0.656" ON ANGLE BELOW RT VORTILON AND LOWER FLANGE, FRONT SPAR AT STA XRS=153.5. DAMAGE WAS REMOVED. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIG 3 AND 51-30-5.

Part: DOUBLER — WORN (FUSELAGE) · airframe 62,259 hrs · 47,425 cycles

WEAR ON PRODUCTION DOUBLER AT FWD UPPER CORNER OF AFT LAVATORY SERVICE PANEL. AREA WAS REWORKED AND WAS FOUND OUT LIMITS AND AREA AT LIMITS WAS REPAIR PERFORMED ER/A 508310-14 REV ORIG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,250 hrs · 47,420 cycles

CRACKS ON EXTERIOR FUSELAGE SKIN AT FWD UPPER CORNER OF FWD SERVICE DOOR. REPAIRED IAW ER/A 508289-14AD, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 927-946) · airframe 62,254 hrs · 47,422 cycles

LIGHTNING STRIKE ON AFT LOWER CORNER OF RT WINDOW BELT FRAME BETWEEN BS 927-946. REPAIR WAS ACCOMPLISHED IAW ER/A 508296-14, REV ORIG.

Part: DOOR FRAME — DAMAGED (BS 655-674) · airframe 62,250 hrs · 47,420 cycles

COROSION ON MID CARGO COMPARTMENT LWR DOOR JAMB BEAM LWR FLANGE AT STA Y=655 AND 674 (C2) IN REF NRC 304 A/C ZONE 51 BEAM OUT OF LIMITS WAS REPAIRED WITH A DOUBLER IAW ER/A 508298-14 REV ORIG.

Part: ANGLE — CRACKED · airframe 62,250 hrs · 47,420 cycles

CRACK OF 0.937 ON ANGLE BELOW LT VORTILON AND LOWER FLANGE, FRONT SPAR AT STA XRS 153.5 REF. NRC (T0 266025). VORTILON ANGLE WAS REPAIRED IAW SRM 57-01 FIG 3.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · airframe 62,250 hrs · 47,420 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1309-1322 AND LONG 27-28 RT. INTERCOSTAL REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SPLICE — CORRODED (BS 1155-1174) · airframe 62,254 hrs · 47,422 cycles

CORROSION ON REPAIR SPLICE ABOVE LONG 25LT BETWEEN STA 1155 AND 1174. ALSO ON STRAP ABOVE SAME ELEMENT BETWEEN STA 1194-1212 AT AFT CARGO COMPARTMENT (C3) REF NRC (T0 265621). SPLICE WAS REPLACED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 1255) · airframe 62,250 hrs · 47,420 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BTW X=-54 TO X=-60 BS 1255 AT PAX CABIN. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: LONGERON SPLICE — CRACKED (BS 1287-1309) · airframe 62,254 hrs · 47,422 cycles

CRACKED LONGERON SPLICE 22 LT BETWEEN BS 1287 TO 1309 AT AFT CARGO COMPARTMENT. LONGERON SPLICE WAS REPLACED IAW IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 1108-1117) · airframe 62,250 hrs · 47,420 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X=-54 TO -60 STA Y=1108 TO 1117. REPAIRED IAW SRM 53-05 FIG 131.

Part: CUSP WEB — CORRODED (BS 1205) · airframe 62,250 hrs · 47,420 cycles

CORROSION ON RT CUSP WEB, X=-54 TO X=-60 BS 1205. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131 A-14.

Part: FRAME — CRACKED (BS 1510) · airframe 62,250 hrs · 47,420 cycles

CRACK ON FRAME BS 1510 . FRAME REPLACED IAW SRM DRD 53-3D, FIG 802 D AND DWG 9911843, REV AC.

Part: FRAME — CORRODED (BS 1380) · airframe 62,250 hrs · 47,420 cycles

CORROSION ON FRAME TEE BS 1380 BETWEEN LONGERON 25L-25R AND ON FRAME FWD CAP. FRAME REPLACED IAW DWG 9912246 REV CE.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · airframe 62,250 hrs · 47,420 cycles

CORROSION ON INTERCOSTAL FROM BS 1309-1322 BTW LONGERONS 27 AND 28L AT AFT CARGO COMPARTMENT (C3). INTERCOSTAL WAS REPLACED & INSTALLED IAW SRM 51-30-2 AND 51-30-5, AND DWG 9936718 REV M.

Part: LONGERON — CORRODED (BS 1212-1252) · airframe 62,250 hrs · 47,420 cycles

CORROSION ON LONGERON 23L FROM BS 1212 TO 1252 AT AFT CARGO COMPARTMENT. AREA OUT OF LIMITS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,250 hrs · 47,420 cycles

CRACKED LONGERON 3L BS 1437. REPAIRED LONGERON IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437 L4R) · airframe 62,250 hrs · 47,420 cycles

CRACKED LONGERON 4R BS 1437. REPAIRED LONGERON IAW SRM 53-02, FIG 18.

Part: SKIN — CRACKED (BS 374) · airframe 62,250 hrs · 47,420 cycles

CRACKS ON FUSELAGE SKIN BS 374 AT FWD UPPER CORNER OF CARGO COMPARTMENT DOOR FRAME, ALSO CRACKED ON INTERNAL PRODUCTION DOUBLER. REPAIR WAS ACOMPLISHED IAW AR/A 508293-14, AD REV ORIG.

Part: FINGER DOUBLER — CRACKED (FUSELAGE) · airframe 62,250 hrs · 47,420 cycles

CRACKED FINGER DOUBLER BS 65 BETWEEN LONGERONS 17 TO 18L. REPAIRED IAW ER/A 498255-14 REV A.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,250 hrs · 47,420 cycles

DAMAGED PAINT AND METALLIZED COAT ON BOTH SURFACES OF RUDDER. METALLIZED COAT ON BOTH SURFACES OF RUDDER WAS REPAIRED AND PAINTED IAW EA 09-461041-03, ME 01.

Part: LONGERON — CRACKED (BS 408 L16L) · airframe 62,250 hrs · 47,420 cycles

CRACK ON LONGERON 16L AT BS 408. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: SKIN — SCRATCHED (BS 1041-1060) · airframe 62,250 hrs · 47,420 cycles

SCRATCH ON AFT LOWER CORNER OF RT WINDOW BELT FRAME BETWEEN STA Y=1041 - Y=1060. REF NRC T0265146. DAMAGE WAS BLENDED OUT, MEASURED, TREATED AND INDENTIFIED IAW ER/A 508295-14 REV. O. ER/A 508295-14 ADDED FOR A/C 0935.

Part: LONGERON — CRACKED (BS 237-256) · airframe 62,250 hrs · 47,420 cycles

CRACKED LONGERON NR 17L AT BS 237 AND 256. DAMAGED SECTION OF LONGERON WAS R & R IAW SRM 53-02, FIG 18.

Part: SKIN — DAMAGED (BS 731-750) · airframe 62,250 hrs · 47,420 cycles

LIGHTNING STRIKE ON AFT MID SECTION OF RT WINDOW BELT FRAME BTW BS 731-750. DAMAGE WAS BLENDED OUT, MEASURED, TREATED AND IDENTIFIED IAW ER/A 508295-14 REV O.

Part: SKIN — DAMAGED (BS 207-229) · airframe 62,250 hrs · 47,420 cycles

DURING HVM4, A DENT WITH SURFACE DAMAGE WAS REPORTED ON AN EXISTING REPAIR DOUBLER LOCATED BETWEEN BS 207-229 AND BETWEEN LONGERONS L16 AND 18L. R & R DAMAGED ELEMENTS WITH NEW ONE FOLLOWING ER/A 508301-14 AND SRM 53-04-5 FIG 3. INSPECT EVERY 8000 CYCLES AFTER 12 NOV 12.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,250 hrs · 47,420 cycles

DURING HMV4 , WHILE PERFORMING MAJOR SKIN REPAIR AT FORWARD CARGO COMPARTMENT DOOR FRAME UPPER FORWARD CORNER, A DOUBLER CRACK WAS FOUND.

Part: LONGERON — CRACKED (BS 1309 L6L) · airframe 62,250 hrs · 47,420 cycles

CRACKED L6L, BS 1309 AT FUSELAGE CABIN STRUCTURE. LONGERON REPAIRED IAW SMR 53-02, PAR 12, GG 18.

Part: LONGERON — CRACKED (BS 1309 L5L) · airframe 62,250 hrs · 47,420 cycles

CRACKED LONGERON 5L BS 1309 FUSELAGE CABIN STRUCTURE. REPAIRED LONGERON 5L IAW SRM 53-02, PAR 12, FIG 18.

Part: LONGERON — CRACKED (BS 160 L2L) · airframe 62,250 hrs · 47,420 cycles

CRACKED LONGERON 2L AT BS 160 REPAIRED IAW SRM 53-02, FIG 18.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 62,250 hrs · 47,420 cycles

LIGHTNING STRIKE ON LT ELEVATOR CONTROL TAB. REPAIRED IAW SRM 55-04, PAR 3C.

Part: TAB — DAMAGED (RT ELEVATOR) · airframe 62,250 hrs · 47,420 cycles

LIGTHNING STRIKE ON RT ELEVATOR GEARED TAB. THE TAB WAS REMOVED. RT ELEVATOR GEARED TAB REPLACED IAW AMM 27-30-04-201.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,433 hrs · 46,834 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION AND BACK TO 12DE OF THE CABIN PLUS BOTH OF THE DOOR EXIT SIGNS AT L1 AND R1 HAD ALL FAILED. MAINTENANCE REPLACED A FAILED FUSE IN THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD.

Part: HINGE BRACKET — CORRODED (VERTICAL STAB) · airframe 61,348 hrs · 46,786 cycles

FOUND CORROSION ON THE SURFACES AND BORES COMMON TO THE VERTICAL TO HORIZONTAL HINGE PLATES. THE PLATES ARE SUBJECT OF SB MD80-55-054 AD 99-07-14 AND EO 09-073278-12AD. SIX OF THE EIGHT HINGE PLATES WERE REPLACED. THE LT OUTBOARD PLATES WERE NOT REPLACED AT THIS TIME.

Part: SPAR CAP — CRACKED · airframe 61,348 hrs · 46,786 cycles

WHILE PERFORMING A SPAR CAP SPLICE REPAIR PER SR09550027 FOR A CRACKED RT UPPER REAR SPAR CAP ON THE DATUM A/C. MAINTENANCE REPORTED ONE FASTENER HOLE LOCATED IN THE FWD FLANGE OF THE SPAR CAP HAS SHORT EDGE MARGIN.

Part: BEAM — CORRODED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

AFT CARGO DOOR BEAM SEAL HAS CORROSION BETWEEN STA 1156 AND 1212. REMOVED CORROSION FOUND BEAM TO BE OUT OF LIMITS PER MD-88 SRM 53-01 FIG 1. REMOVED AND REPLACED AFT CARGO LOWER DOOR SEAL BEAM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

CORROSION ON LONGERON 23L BETWEEN STA 1296 AND 1315. CUT OUT DAMAGED SECTION OF LONGERON AND INSTALLED NEW SECTION AND SPLICE PER THE MD-88 SRM 53-01 AND ER/A 497805-14 REV ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

N/R 191 INTERIOR SKIN SURFACE CORROSION C-3 CARGO DOOR CUTOUT STA 1165 AT LONGERON 27R. N/R 209 INTERIOR SKIN SURFACE CORROSION C-3 CARGO DOOR CUTOUT STA 1173 AT 27R. ACCOMPLISHED REPAIRS PER ERA 498309-14 REV ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

DURING PSV VISIT NRC_53 FASTENERS POPPED AND SKIN HAS CORROSION ALONG LOWER EDGE OF AFT LAV SERVICE PANEL. STA 1307 AT L 22L.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

DENT FOUND ON SKIN AT FS 58 LT SIDE AT LBL 0 JUST FWD AND ABOVE AOA VANE. INSTALLED TIME LIMITED REPAIR PER SRM 53-04 FIG 12 AND ER/A 498255-14 REV 0.

Part: SKIN — DAMAGED (FS 1307 L22L) · airframe 60,229 hrs · 46,031 cycles

FUSELAGE SKIN STA 1307 L22L SURROUND DOUBLER AFT LAVATORY. SERVICE DOOR CUTOUT REPAIR IAW ER/A 498213-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

DURING PSV IN MSP MTC NOTED CORROSION BETWEEN THE FUSELAGE SKIN AND THE INTERNAL DOUBLERS COMMON TO THE C3 CARGO DOOR SURROUND BELOW THE JAMB BEAM. REPAIRED PER ER/A 498299-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

DURING PSV IN MSP MTC NOTED FLOOR SUPPORT TEE CORRODED AT STA 1135 TO 1211 L28. TEE REPLACED PER MD88 SRM 53-01.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,229 hrs · 46,031 cycles

DURING PSV IN MSP MTC NOTED WEB AND STRAPS CORRODED DURING REPLACEMENT OF C3 CARGO BEAM. REPLACED WEB PER MD88 SRM 53-01.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 60,103 hrs · 45,933 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY AISLE LIGHT AT ROW 11 RIGHT INOPERATIVE. MAINTENANCE REPINNED THE CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 59,646 hrs · 45,594 cycles

DURING LINE CHECK MAINTENANCE FOUND RED EMERGENCY LIGHT ON FORWARD GALLEY WALL INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT 1D PER WSPM CHAPTER 20. OPERATION OF LIGHTS CHECKS OK.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 58,920 hrs · 45,056 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 22DE. MAINTENANCE FOUND HARNESS BETWEEN LIGHT AND SIDEWALL BAD. REMOVED AND REPLACED SAME PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 58,772 hrs · 44,954 cycles

DURING LINE CHECK, MX FOUND FWD CABIN EMERGENCY LIGHTS INOPERATIVE. MX FOUND FWD CABIN EMERGENCY POWER PACK FUSES BURNED AND A BROKEN WIRE AT ROW 4CD. MX REPLACED LIGHT ASSY AND FUSE FOR POWER PACK. OPS CHECKS NORMAL.

Part: LANYARD — MISROUTED (L2 DOOR) · airframe 58,684 hrs · 44,889 cycles

DURING LINE CHECK MAINTENANCE FOUND L2 DOOR SLIDE LANYARD WAS MIS-ROUTED AND FRAYED. MAINTENANCE REPLACED SLIDE LANYARD PER M/M.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,394 hrs · 44,695 cycles

FUSELAGE FRAME 1451 LONGERON 1 CRACK REPAIR. REPAIRED PER ERA 489679-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,394 hrs · 44,695 cycles

FUSELAGE SKIN STA 1418 LONG 1R TO 2R CRACKED. REPAIRED PER ERA489507-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,271 hrs · 44,614 cycles

FUSELAGE SKIN CRACK STA 1437 LONG 2L TO 3L AND 2R TO 4R. REPAIRED PER ERA 489508-14.

Part: OIL CAP — LEAKING (APU) · airframe 57,994 hrs · 44,437 cycles

THE FLIGHT RETURNED TO LGA DUE TO SMOKE IN THE CABIN WITH LAVATORY SMOKE DETECTORS SOUNDING AFTER TAKEOFF. MAINTENANCE FOUND AN APU OIL LEAK AT THE CAP AND REPLACED IT. THE APU INLET AND EXTERNAL AREAS WERE CLEANED AND OPERATION 5089 DUCT BURN OUT PROCEDURES WERE ACCOMPLISHED. (2010-D1397) (DLM88103254)

Part: SKIN — DENTED (FUSELAGE) · airframe 56,200 hrs · 43,176 cycles

FOUND ON ARRIVAL LARGE DENT AFT OF L1 DOOR LWR RIGHT. DENT IS IN EXISTING DOUBLER FROM PREV REPAIR. REMOVED DOUBLER AND FORMER CLIP AT FLOOR LINE STA 237. INSTALLED FORMER CLIP AT FLOOR LINE. FABRICATED REPAIR PIECES PER SRM 53-04-05. OK TO INSTALL REPAIR PER SRM 53-04-05 AT STA 237 LONGERON 18L TO 20L QC1502. INSTALLED REPAIR DOUBLER ABOVE FLOOR LINE AT 2TA 237 PER SRM 53-04-05. INSPECT REPAIR.

Part: SKIN — CRACKED (BS 617 L30) · airframe 55,717 hrs · 42,846 cycles

FUSELAGE SKIN BS 617 AND L30 CRACK AND CORROSION REPAIR IAW ER/A 478781-14.

Part: CLEVIS — BROKEN (AIRSTAIR DOOR) · airframe 54,607 hrs · 42,096 cycles

AT FL 330 HEARD LOUD BANG IN AREA OF FWD GALLEY. FLOW LIGHT ILLUMINATED AND CABIN STARTED CLIMBING RAPIDLY. DESCENDED TO FL 210. CABIN STABILIZED FOR 10 MINUTES. FLOW LIGHT THEN RE-ILLUMINATED AND CABIN STARTED CLIMBING AGAIN. DESCENDED TO 10,000 FT AND DIVERTED. LANDING WAS NOT OVERWEIGHT. FOUND AFT CLEVIS OF FWD STAIR DOOR BROKEN. REPLACED SAME, REF MM. PRESSURIZED A/C, NO LEAKS NOTED.

Part: SKIN — CORRODED (FS 363 L29-30R) · airframe 52,366 hrs · 40,625 cycles

SKIN CORROSION AT FS 363-370, L-29R-L30. CORROSION WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: BLANKET — SHORTED (RT WING) · airframe 51,814 hrs · 40,264 cycles

WHILE INSTALLING RT WING HEATER BLANKET MTC DRILLED AFT HOLES PRIOR TO VACUUM BAGGING AS CALLED FOR IN AMM. ER/A ISSUED TO AUTHORIZE DRILLING THE HOLES PRIOR TO BAGGING.

Part: RESERVOIR — AERATED (HYD SYSTEM) · airframe 50,398 hrs · 39,393 cycles

LEFT HYD SYS PRESS READ ZERO/QTY READ 16QTS WHILE, AIRBORNE 19QTS AT TAXI IN PRESS DROPPED TO ZERO SHORTLY AFTER SLATS WERE EXTENDED. ON ARRIVAL, BLED LT SYS HYD FOUND ABNORMAL AMOUNT OF AIR IN SYS. EXERCISED FLT CONTROLS AND BLED MORE AIR FROM LT SYS. RAN ENG AND PRESSURIZED LT AND RT HYD SYS. LT ENG PUMP PRESS NORMAL. RAN FLT CONTROLS AND CK OK.

Part: TERMINAL BLOCK — BURNED (APU FEEDER CABLE) · airframe 50,133 hrs · 39,208 cycles

AIRCRAFT HAS ELECTRICAL SMELL IN CABIN. FOUND APU FEEDER CABLE TERMINAL BLOCK BURNED BELOW CIRCUIT BREAKER PANEL BEHIND CAPTS SEAT. REMOVED TERMINAL BLOCK. FEE CABLE NEEDS RETERMINATED. REPLACED TERMINAL BLOCK S3-23 AND REPAIRED FEEDER CABLE 3X1B00AAL PER BSWPM CH 20. APU OPN AN APU ELECTRICS CK NML ACFT. OK FOR SVC.

Part: SKIN — DELAMINATED (T\E FLAP VANE) · airframe 47,618 hrs · 37,509 cycles

REPAIR OF RT INBD FLAP/INBD VANE - TWO AREAS OF DELAMINATION ON THE L/E SKIN AND ONE ON THE LOWER SURFACE BETWEEN STAXIVIF=6.2364 AND XIVIF=35.5571. PERMANENT REPAIRS INSTALLED PER AEROMEXICO REPAIR DRAWING NR AMR0957141 R03 DATED 24AUG06 VIEW C AND REPAIR SKETCH SK-06-170/CFLCH DATED 05OCT06. REF ERA 457446-14.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 47,611 hrs · 37,504 cycles

LT WING INBD FLAP LOWER SKIN P/N 9935942-5 REPAIR - EXISTING REPAIR FOUND ON L/H WING INBD FLAP LOWER SKIN PANEL. DATA SENT TO BOEING FOR APPROVAL. BOEING REQUESTED INSTALLATION OF ADDITIONAL REPAIR SPLICE ON INTERNAL REB AT STA XIFO=110.608. REPAIR SPLICE INSTALLED PER ERA 458263-14. REMAINDER OF REPAIR APPROVED BY BOEING MESSAGE NO 1-239801280-6.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,611 hrs · 37,504 cycles

FUSELAGE SKIN REPAIR AT STA Y=160 BETWEEN LONGERONS 20 AND 22L - FUSELAGE SKIN CRACKED. REPAIRED PER BOEING REWORK DRAWING SR-09530219-7001 AND IAW EA 09-069085-12AD.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 47,608 hrs · 37,502 cycles

RT INBD FLAP, REMOVABLE SECTION, LOWER SKIN REPAIR - TWO TEMP REPAIRS FOUND ON FLAP PANEL P/N 9935942-6. PERMANENT REPAIRS INSTALLED PER AM REPAIR DRAWING AMR0957173 R01 AND ERA 457448-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,608 hrs · 37,502 cycles

REPAIR IN FUSELAGE SKIN BETWEEN STA Y=1079 AND 1117 AT L29L TO L29R - SEVERE CORROSION FOUND IN TWO AREAS AROUND DRAIN HOLES LOCATED IN THE LOWER FUSELAGE SKIN P/N 5936022-29. REPAIRED PER AM REPAIR DRAWING AMR0953559 R1 AND ERA 457450-14.

Part: SKIN — DELAMINATED (TE FLAPS) · airframe 47,603 hrs · 37,499 cycles

DURING VISIT, TWO AREAS OF DELAMINATION WERE FOUND IN THE SKIN LOWER SURFACE. AREAS REPAIRED PER BOEING INSTRUCTIONS, SEE ERA 457446-14

Part: SKIN — CORRODED (FS 1079-1117) · airframe 47,601 hrs · 37,498 cycles

DURING CURRENT HMV VISIT AT GDL, SEVERE CORROSION WAS REPORTED IN TWO AREAS, DRAWING HOLES, BETWEEN 1079 AND 1117, BEWTEEN L-29L AND L-29R. THE DAMAGE WAS REMOVED BY CUTOUT AND AND A BOEING APPROVED REPAIR INSTALLED PER 457450-14

Part: TEE FITTING — DAMAGED (BULKHEAD) · airframe 47,601 hrs · 37,498 cycles

DURING THE CURRENT MTC CHECK EO 09-086680-12 WAS BEING ACCOMPLISHED AND THE REPLACEMENT PRESSURE BULKHEAD TEE CHORD WAS FOUND TO HAVE SHORT EDGE MARGIN ON EXISTING FASTENERS DURING INSTALLATION. DUE TO THIS, A TITANIUM REPAIR STRAP APPROVED BY MFG IS INSTALLED IAW ERA 458260-14.

Part: WIRE — BROKEN (CABIN FLOOR) · airframe 44,531 hrs · 35,390 cycles

DURING TAXI OUT AND WHILE ON TAXIWAY PASSENGER AT SEAT ROW 28 NOTICED LOOSE WIRING UNDER SEAT ROW 27. AIRCRAFT RETURNED TO RAMP AREA AND MTC DISCOVERED EMERG TRACK LIGHTING WIRE PULLED AWAY FROM SIDEWALL WITH ONE WIRE BROKEN. MADE APPROVED REPAIR TO WIRING AND SECURED SAME BEHIND SIDEWALL. EMERG TRACK LIGHTING OPERATES NORMALLY THROUGHOUT CABIN.

Part: TIRE — FAILED (NR 3 MLG) · airframe 44,516 hrs · 35,380 cycles

ON T/O FLT ATTENDANT REPORTED NOISE FOLLOWED BY SMELL OF BURNT RUBBER. CREW HAD RETRACTED GEAR AND ON EXT HAD RED UNSAFE LIGHT. MAIN TIRE THREW A CAP. TIRE WAS STILL INFLATED 200PSI SOME DAMAGE TO FLAP, MLG DOWN LOCK CONDUIT AND SENSOR/BRACKET, BUTE DOOR AND NR 2 ENGINE FAN. REPLACED WHEEL AND REPAIRED DAMAGE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 42,759 hrs · 34,086 cycles

AFT CABIN EMERGENCY AISLE LIGHTS INOP. FOUND BROKEN WIRE AT LIGHT ASSY L2-846 AND REPLACED INOP PWR SUPPLY B5-212.

Part: LINK — BROKEN (NLG) · airframe 42,334 hrs · 33,778 cycles

SEVERE VIBRATION FROM NOSE GEAR AREA ON TAKEOFF. FOUND LT NOSE GEAR DOOR LINK BROKEN. REPLACED LINK, CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 41,029 hrs · 32,842 cycles

AFT STAIRWAY CENTER EMERGENCY LIGHT MISSING LENS AND INOP. REPLACED LENS AND BATTERY PACK.

Part: SWITCH — OUT OF ADJUST (HORIZONTAL STAB) · airframe 38,089 hrs · 30,796 cycles

STABILIZER CONFIGURATION WARNING. ABORTED TAKE OFF AT 70 KTS. FOUND HORIZONTAL STAB TAKE OFF WARNING SWITCH OUT OF ADJUSTMENT. PERFORMED ADJUSTMENT &TEST PER M/M 27-40-00-05. ALL CHECKS NORMAL NOT RII. OK FOR SERIVCE.

Part: INDICATOR — OBSTRUCTED (COCKPIT) · airframe 37,054 hrs · 30,065 cycles

CABIN ALTITUDE CONTROL JAMMED INFLIGHT. CABIN ALTITUDE EXCEEDED 14,000 FEET. MASKS DEPLOYED. EMERGENCY RETURN TO DFW. FOUND LOOSE HARDWARE OBSTRUCTING MOVEMENT OF OUTFLOW VALVE INDICATOR ON PEDESTAL. REMOVED HARDWARE. RAN BITE OF AUTO PRESSURIZATION CONTROLLERS. BITE CHECKS NORMAL. REPLACING OXYGEN GENERATORS AND MASKS.

Part: PITOT LINE — LOOSE (E/E BAY) · airframe 37,033 hrs · 30,051 cycles

F/O AIRSPEED WENT TO ZERO, A/T AND A/P DISCONNECTED, OVERSPEED WARNING CONTINUOUS, F/D FAILED, F/O AIRSPEED WENT FROM 0 KTS TO 350 KTS. CADC BOTH ON 1 AIRSPEED, RETURNED TO NORMAL. FOUND PITOT LINE AT NR 2 CADC NOT SECURED. AS PRECAUTION REPLACED NR 2 CADC PER M/M 34-16-01-2. RAN RTS BOTH NR 1 AND 2 DFGC SYSTEMS GO.

Part: AILERON — STIFF (WINGS) · airframe 37,032 hrs · 30,050 cycles

DURING CLB-OUT EWR PILOT NOTED AILERONS FELT VERY STIFF. AILERON REPONSE WAS NORMAL. FLIGHT RETURNED TO EWR. PILOT REPORTED AILERON FELT NORMAL ON APPROACH TO EWR. MTC INSPECTED AILERON SYSTEM WITH NO OBVIOUS DEFECTS NOTED. LUBRICATED AIL ERON MECHANISM IN MAIN WHEEL WELL. FLT CONTROL CHECK NORMAL.

Part: SENSOR — FAILED (HORIZ STAB) · airframe 36,342 hrs · 29,508 cycles

PRIMARY TRIM RAN AWAY NOSE UP. AIRCRAFT RETURN TO B-13. REPLACED STAB MOTION SENSOR C/W ADJ/TEST PER MM 27-40-04-5 AND 27-40-02-2 AND VISUALLY INSPECTED STAB JACKSCREW, NTF.

Part: PANEL — MISSING (AILERON TAB) · airframe 34,328 hrs · 28,010 cycles

CLOSE OUT PANEL FOR AILERON TRIM TAB O/B BEARING TOP COVER MISSING. REPLACED SAME.

Part: ENGINE — FAILED (NR 2) · airframe 34,177 hrs · 27,897 cycles

AFTER CLIMBOUT PASSING THRU 1000 FEET LOST THE RIGHT ENGINE. ENGINE SEIZED, NO RELIGHT WAS ATTEMPTED. REPLACED ENGINE.

Part: HANDLE — FAILED (COCKPIT) · airframe 33,354 hrs · 27,294 cycles

UNSAFE GEAR LIGHT IND ON ALL 3 GEARS. FOUND GEAR HANDLE NOT FULLY DOWN. PERFORMED GEAR EXT, RET TEST PER M/M. CHECKS GOOD.

Part: TIRE — FAILED (NR 4)

ON T/O PVD NR 4 MLG TIRE TREAD SEPARATED AND TREAD SUBSEQUENTLY INGESTED INTO RIGHT ENGINE. REPLACED WHEEL ASSY AND ENGINE.

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE)

ON CLIMB-OUT, BETWEEN FL240 - FL290, 3 OCCURANCES OF A LOUD NOISE IN AFT CABIN, COMBINED WITH A SHORT PRONOUNCED AIRCRAFT VIBRATION FELT THROUGHOUT THE ENTIRE ACFT, AS WELL AS THE CONTROL COLUMN. DID NOT NOTE ANY ABNORMAL ENGINE INDICATIONS OR MESSAGES. BOROSCOPE OF ENGINE REVEALED COMPRESSOR DAMAGE. REPLACED NR 2 ENGINE.

Part: ACTUATOR — FAILED (RT MLG)

TAKEOFF ROLL, BRAKE TEMP LIGHT AND GAUGE FLICKERED ON/OFF AND READ HIGH TEMP. RAISED GEAR AND GOT RT MAIN UNSAFE AND GEAR DOOR LIGHT. OTHER GEAR UP AND LOCKED. CYCLED GEAR AND GOT SAME INDICATION. CAN FEEL/HEAR GEAR DOOR RUMBLE AT CRUISE. REPLACED RT MLG RETRACT ACTUATOR LOWER ATTACH FITTING AND LOWER PIN PER MM 32-32-02, OPERATION NORMAL.

Part: CONTROL CABLE — DISCONNECTED (ELEVATOR)

WHILE TAXIING OUT DURING FLT CONTROL CHECK, PILOT REPORTED ELEVATOR CONTROL FELT ABNORMAL. RETURNED TO BLOCK AND FOUND HORIZONTAL STAB TRIM CABLE TURNBUCKLE UNDONE AT THE ELEVATOR FEEL FORCE LIMITER. REATTACHED CABLE, CHECKED OPERATION PER MM 27-30-00, OPERATION NORMAL.

Part: SKIN — CRACKED (LT NOSE)

FOUND DURING A-1 LETTER CHECK, .5 INCH LONG CRACK FOUND ON FUSELAGE SKIN AT THE AFT HINGE CUTOUT OF LT NOSE WHEEL WELL DOOR. REPAIRED PER SRM 53-05 FIG 62.