N961DL

Part: RIB — CRACKED (NR 2 NOSE COWL) · airframe 74,569 hrs · 55,732 cycles

#2 ENG NOSE COWL HAS A CRACKED SUPPORT RIB @ 6 O'CLOCK POS. R & R NBR 2 ENG NOSE COWL, REF CARD 7100-4680. (LP0814998)

Part: SERVICE PANEL — CRACKED (LAVATORY) · airframe 74,569 hrs · 55,732 cycles

AFT LAV SERVICE PANEL LOWER CORNER 1/2 INCH SKIN CRACK. REPAIRED PER ERA 572732-14 REV. ORIG. C/W RII QC3032. (LP4586680)

Part: BATTERY PACK — FAILED (CABIN) · airframe 74,511 hrs · 55,683 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT AFT EMERGENCY EXIT SIGNS NOT ILLUMINATING. TROUBLE SHOOTING PER WDM 33-51-12 AND 33-51-14 ALLOWED DISCOVERY THAT THE EMERGENCY LIGHT BATTERY PACKS B5-105 AND B5-212 HAD FAILED. BOTH BATTERY PACKS WERE REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP 4586658)

Part: ENGINE — SMOKE (NR 1) · airframe 73,686 hrs · 54,968 cycles

FUMES IN COCKPIT AND CABIN WHILE SMOKE REPORTED BY OTHER AIRCRAFT FROM ENG NR 1 ON GROUND AFTER 2.5 HOUR TAXI GATE RETURN. REMOVED AND REPLACED LT AND RT WATER SEPARATOR/COALESCER BAGS REFERENCE AMM 21-20. REPLACED NR 1 ENGINE. PERFORMED NO GO ODI PREVENTION ATA 2172 WORK CARD 2120-2367, 2120-2368, 7100-2619. FOUND NO EVIDENCE OF TURBO OIL IN IN ANY PNEUMATIC DUCTS. DUCT BURNOUT PERFORMED RAN ENGINES & A/C PACKS NO FUMES PRESENT A/C OK FOR SERVICE.

Part: PAN — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 73,374 hrs · 54,722 cycles

CORROSION AROUND ON INTERNAL SKIN AT FWD TOILET PANEL. LEVEL CORROSION 2. PAN AT FWD LAVATORY ACCESS PANEL WAS REPLACED PER SRM 51-30-2, 51-30-5.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 73,374 hrs · 54,722 cycles

DURING FASTENER REMOVAL, HOLES WERE FOUND ELONGATED ON L/E AT VERTICAL STABILIZER JUST ABOVE RAM AIR INLET STA ZFS 17.66 APPROX VERTICAL STABILIZER LEADING EDGE SKIN AT ZFS=17.66 WAS REPAIRED PER ETI-88-18-046 REV 8 AND ER/A568315-14 REV ORIGINAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,752 hrs · 53,422 cycles

AFT OVERWING EXIT LIGHTS INOP. R&R BATTERIES IN B-5105. OPS CK SAT AMM 33-53.

Part: WIRE — DAMAGED · airframe 70,658 hrs · 52,576 cycles

FOUND A WIRES DAMAGED . REPAIRED THE WIRES IAW WDM 33-24, 52-73, 25-41, 35-24, AND 33-21. TESTED SYSTEMS IAW WDM. ALL TESTED GOOD.

Part: WIRE — DAMAGED · airframe 70,658 hrs · 52,576 cycles

FOUND WIRES DAMAGED - WDM 21-31. REPAIRED THE WIRES IAW WDM. TESTED IAW WDM 21031, 33-23, & 33-38. ALL TESTED NORMAL.

Part: WIRE — CHAFED (CABIN OVERHEAD) · airframe 70,658 hrs · 52,576 cycles

AFTER ARRIVAL AT THE GATE, WITH ONLY THE APU POWERING THE AIRCRAFT, SPARKS AND FLASHING LIGHTS WERE REPORTED IN THE FIRST CLASS OVERHEAD CEILING AREA. THE PASSENGER OXYGEN MASKS DEPLOYED AND SMOKE WAS DETECTED IN THE FLIGHT DECK. SEVERAL FLIGHT DECK CIRCUIT BREAKERS TRIPPED. WIRES WERE FOUND CHAFED AND SHORTED IN THE CABIN OVERHEAD CEILING. THE WIRES WERE IDENTIFIED, ISOLATED, AND REPAIRED.

Part: WIRE — DAMAGED (CABIN LIGHTS) · airframe 70,658 hrs · 52,576 cycles

FOUND WIRES DAMAGED IAW WDM 33-22. REPAIRED THE WIRES IAW WDM 33-22.

Part: WIRE — DAMAGED · airframe 70,658 hrs · 52,576 cycles

TRANSFORMER TRAY ASSEMBLY IN CEILING NEXT TO FWD LAV DOOR HAS SIGNS OF ARCHING CAUSED BY WIRE DAMAGE PASSING OVER IT. REPAIRED IAW RI 556663-14.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 70,658 hrs · 52,576 cycles

DURING THE LANDING ROLL, THE CREW REPORTED THE BRAKES FELT LIKE THEY WERE CYCLING AND THE AIRCRAFT WAS NOT SLOWING DOWN. MAINTENANCE BLED THE BRAKES IAW AMM 32-42 AND RETURNED THE AIRCRAFT TO SERVICE.

Part: ANGLE — BROKEN (BS 1463 BULKHEAD) · airframe 70,524 hrs · 52,470 cycles

BROKEN ANGLE AT RT SIDE CANTED BULKHEAD BS 1463. REMOVED, FABRICATED, PRIMED, PAINTED AND INSTALLED IAW DWG 9911839. OK FOR SEVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 70,187 hrs · 52,223 cycles

MULTIPLE CEILING EMER LIGHTS OUT IN F/C & TAIL COMPARTMENT. R&R B5-28 POWER SUPPLY REF MM 33-53. OPS CKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 69,698 hrs · 51,862 cycles

EMERGENCY LIGHT AT SEAT 17D HAD A WIRE IS BROKEN. SECURED THE WIRE AND REPLACED THE LAMP. OPS CHECKED GOOD.

Part: TURBINE — DAMAGED (NR 1 ENGINE) · airframe 69,493 hrs · 51,680 cycles

FLIGHT RETURNED TO DEPARTURE WITH A REPORTED ENGINE ISSUE. PILOT REPORTED BANG ON TAKEOFF. NR 1 ENGINE PARAMETERS DECLINED TO ZERO WITH EGT INCREASING. ENGINE SHUTDOWN. MAINTENANCE FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. ENGINE CHANGE COMPLETED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,680 hrs · 51,059 cycles

EMERGENCY EXIT LIGHTS BETWEEN ROWS 17 & 20 ARE INOPERATIVE. R & R BATTERIES IN EMERGENCY LIGHTS PACK AT ROW 17 IAW AMM 33-53. EMERGENCY LIGHTS, OPS CHECK GOOD OK FOR SERVICE.

Part: DOUBLER — CORRODED (BS 1380) · corrosion level 2 · airframe 68,417 hrs · 50,871 cycles

DOUBLER CORRISION AT BS 1380, APB, L29 AFT SIDE OF WEB. R & R ANGLE, PN 9915561-73 REF PRI 545891-14, REV 0 AND REPAIR ERA 545891-14, REV ORIGINAL.

Part: BULKHEAD — CRACKED (BS 37) · airframe 68,417 hrs · 50,871 cycles

FUSELAGE NOSE, CRACK IN BULKHEAD SKIN, BS 37, RADOME GUIDE PIN 3 O'CLOCK POSITION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0279:5300-2128/001 00144. REPAIRED REF ERA 420243-14MA, REV B.

Part: FRAME — CRACKED (TAILCONE) · airframe 68,417 hrs · 50,871 cycles

CANTED FRAME BS 1510 CRACKED AT TAILCONE ALIGNMENT PIN AT 2 O'CLOCK. REPAIRED IAW PRI 546574-14, REV 1 AND COMPLIED WITH ER/A 546574-14, REV ORIGINAL.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 68,417 hrs · 50,871 cycles

AFT CARGO DOOR SILL, CORROSION ON FWD LOWER CORNER. INSTALLED INTERNAL SILL PLATE IAW AMM 25-52-01, PB 201. ALL REPAIR WORK PERFORMED AND COMPLETED IAW ER/A 499523-14MA, REV ORIGINAL AND SRM 53-05, FIG 123.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 68,341 hrs · 50,821 cycles

THE CREW PERFORMED AN AIR TURN BACK DUE TO WINDSHEAR AND SUBSEQUENT DUAL ENGINE OVERSPEED. THE CAPTAIN FIREWALLED BOTH ENGINES AND BOTH WENT TO 2.2 EPR FOLLOWED BY COMPRESSOR STALLS AND AN ODOR IN THE CABIN. DURING INITIAL CLIMB-OUT CAPTAIN NOTICED AIRSPEED DECAY TO V2 +10 AND MENTIONED LOWERING NOSE TO GAIN AIRSPEED. AT APPROXIMATELY 1000 FEET AGL AIRSPEED DECAYED TO V2 AND CREW RECEIVED WINDSHEAR WARNING. THE NR 1 ENGINE N1 110 PERCENT EGT 680, THE NR 2 ENGINE N1 105 PERCENT EGT 645. REPLACED NR 1 ENGINE. REPLACED NR 2 ENGINE FAN.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,819 hrs · 50,474 cycles

THE CREW REPORTED THAT THE OVERWING EXTERIOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 67,556 hrs · 50,265 cycles

MAINTENANCE FOUND SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT 25D, 26D, AND 17D. THE EMERGENCY LIGHT HARNESSES AND OR PIGTAILS WERE REPLACED AT 25D, 26D, AND AND 17D AND LIGHTS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 67,222 hrs · 50,032 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 26D IN THE CABIN WAS INOPERATIVE DUE TO A BROKEN WIRE. MAINTENANCE FOUND A LOOSE WIRE IN THE CONNECTOR, RE-INSTALLED THE WIRE INTO THE CONNECTOR, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,452 hrs · 48,810 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR 12 SEATS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 63,015 hrs · 47,099 cycles

DURING A CHECK OF TAILCONE, MAINTENANCE FOUND THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.

Part: SKIN — CRACKED (BS 1418) · airframe 63,013 hrs · 47,098 cycles

CRACK OF 0.125" ON FUSELAGE SKIN AT BS 1418 BETWEEN LONGERONS 2-3L. REPAIRED IAW ER/A 521196-14AD.

Part: CARGO TRACK — CORRODED (BS 1003-1225) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON RT CARGO TRACK FROM BS 1003 TO 1155 AND BS 1003 TO 1225. REPLACED CARGO TRACK IAW 51-10-3, 51-10-4 AND 51-30-1.

Part: ATTACH FITTING — CRACKED (BS 927) · airframe 63,013 hrs · 47,098 cycles

CRACK ON LONGERON ATTACH BS 927 AND L6R AT AFT CEILING PAX CABIN STRUCTURE. REPAIRED IAW SRM 53-02, FIG 18, SRM 51-10-4, 51-10-03, PAR 14 & 21 AND SRM 53-14-03.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON EDGE OF FLOOR PANEL IN AFT CARGO BAY. REPLACED FLOOR PANEL.

Part: ATTACH FITTING — CRACKED (BS 927) · airframe 63,013 hrs · 47,098 cycles

CRACK ON LONGERON ATTACH BS 927 L6L AT AFT CEILING PAX CABIN STRUCTURE. REPAIRED IAW SRM 53-02, 51-10-04, 51-10-03 AND 53-14-03.

Part: WEB — CORRODED (BS 180-200) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON WEB BETWEEN BS 180-200 AND X -34 TO X-60. REPAIRED IAW SRM 51-70-4, FIG 2.

Part: WEB — CORRODED (BS 200-218) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON WEB BETWEEN BS 200-218, X-44 TO X -60 AT PAX CABIN FLOOR STRUCTURE. REPAIRED IAW SRM 51-70-4, FIG 2.

Part: ANGLE — CORRODED (BS 180-200) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON RT CUSP ANGLE BETWEEN BS 180 AND 200 X=-58 . RT CUSP ANGLE REPAIRED IAW SRM 53-05, FIG 55 AND ER/A 521188-14MA, REV ORIGINAL.

Part: INTERCOSTAL — CORRODED (BS 1136-1155) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON INTERCOSTAL FROM BS 1136 TO 1155 ABOVE LONGERON 29L. REPLACED IAW SRM 51-10-3, PAR 14, 21, 38, SRM 51-30-5.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON FRAME PREVIOUS REPAIR BS 1309, BETWEEN LONGERONS 29L-29R. PREVIOUS REPAIR REMOVED IAW SRM 53-03D, FIG 2-A. NEW REPAIR INSTALLED IAW SRM 53-03D, FIG 2-A.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,789 hrs · 51,938 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AND TRIPLER OF RT CUSP WEB STA Y=715 AND Y=728.5 FROM X= -55 AND X= -60 FLOOR CABIN STRUCTURE. DOUBLER & TRIPLER WERE REMOVED, REPAIR PARTS WERE FABRICATED , TRIMMED, DRILLED, TREATED & PAINTED AND INSTALLED.

Part: SKIN — CORRODED (BS 648-662) · airframe 63,013 hrs · 47,098 cycles

NON ROUTINE CHECK, CORROSION FOUND ON PREVIOUS REPAIR ON MID CARGO BAY LOWER DOOR FRAME BEAM BETWEEN BS 648-662. REPAIR REMOVED IAW SRM 51-30-5, NEW SPACER REPAIR WAS FABRICATED IAW SRM 53-05, FIG 123, TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14, FABRICATED NUT STRIP IAW SRM 53-05, FIG 23, TREATED AND PAINTED IAW SRM 51-10-3, PAR 21,14. NEW SPACER REPAIR AND NUT STRIP INSTALLED IAW SRM 51-30-5.

Part: SKIN — DAMAGED (BS 788-807) · airframe 68,370 hrs · 50,836 cycles

AT HMV4, A BS 788-807, LT WINDOW BELT LIGHTNING STRIKE WAS REPAIRED IAW ERA 521186-14, SECT 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,789 hrs · 51,938 cycles

CORROSION ON RT CUSP WEB X=-54 TO X=-60 AT STA Y=635 AND BTW STAY=676 TO 678 FLOOR CABIN STRUCTURE. REPAIR PARTS WERE FABRICATED, TREATED/PAINTED AND REPAIR PART WAS INSTALLED IAW SRM 53-01 FIG 4.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,789 hrs · 51,938 cycles

CORROSION ON RT CUSP WEB BTW STA Y=1016 TO 1019 AND Y=1030 TO 1032. REPAIR PARTS WERE FABRICATED IAW SRM 53-05 FIG 131A, TREATED/PAINTED AND INSTALLED IAW SRM 53-05 FIG 131A.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,789 hrs · 51,938 cycles

CUSP WEB CORROSION LWR SURFACE STA Y=635, BETWEEN X=-54 TO -60, AT FLOOR CABIN STRUCTURE. PARTS FABRICATED AND REPLACED.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 69,789 hrs · 51,938 cycles

CORROSION ON RT CUSP WEB UPPER/LOWER SURFACE STA Y=676 TO Y=678 BTW X=-54 TO X=-60 AT FLOOR CABIN STRUCTURE. REPAIR PARTS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW 53-01 FIG 4.

Part: CUSP WEB — CORRODED (BS 848-861) · airframe 63,013 hrs · 47,098 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AND TRIPLER OF RT CUSP WEB, BS 848.5 AND 861 BETWEEN X=-55.5 AND X=-60. DOUBLER DAMAGE WAS REMOVED IAW SRM 51-30-5. NEW DOUBLER FABRICATED AND INSTALLED IAW ERA 398191-14MA. REV B,

Part: CARGO TRACK — CORRODED (BS 1007-1220) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON LT CARGO TRACK FROM BS 1007-1220 AT AFT CARGO BAY. CARGO TRACK REMOVED, & NEW CARGO TRACK WAS DRILLED, TREATED AND PAINTED, INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, 51-10-3.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 63,013 hrs · 47,098 cycles

NON ROUTINE CHECK, FOUND DAMAGED FLAME SPRAY ON RUDDER. REPAIRED IAW SRM 51-70-1AD.

Part: CUSP WEB — CORRODED (BS 1188-1191) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON LT CUSP WEB UPPER & LWR SURFACES BETWEEN BS 1188 AND 1191 FROM X=54 TO X=60. DAMAGE WAS REMOVED, REPAIR FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-05, FIG 131-A7, SRM 51-10-3, PAR 21, 14, 38.

Part: BULKHEAD — CORRODED · corrosion level 2 · airframe 69,743 hrs · 51,903 cycles

CORROSION MOVABLE CEILING AFT BULKHEAD AT AFT ACCESORIES COMPARTMENT. BULKHEAD AT AFT ACC COMPARTMENT WAS REMOVED IAW SRM 51-30-1 AND 51-30-8 NEW BULKHEAD WAS FABRICATED; TREATED AND PAINTED IAW SRM 53-14-3FIG 9 51-10-3 PAR 21 AND 14 NEW BULKHEAD WAS INSTALLED IAW SRM 51-30-1,51-30-2 AND 51-30-8.

Part: FLOORBEAM — CORRODED (BS 1338) · corrosion level 2 · airframe 69,743 hrs · 51,903 cycles

CORROSION ON FLOORBEAM BS 1338, X 38. DAMAGE WAS REMOVED, REPAIR FABRICATED, ADJUSTED, INSTALLED, AND CIC APPLIED,IAW SRM 53-05 FIG 20A, 51-10-4, 51-10-3 PAG 14,21,38,PS 900-1-5.

Part: CUSP WEB — CORRODED (BS 525-564) · corrosion level 2 · airframe 69,698 hrs · 51,862 cycles

CORROSION ON RT CUSP WEB X -54 TO X -60 AND BS 525 - 564. REPAIRED IAW SRM 53-05 FIG. 131A-14 (SHEET 1).

Part: FRAME — CORRODED (BS 1271) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION FOUND ON FRAME, BS 1271 BETWEEN LONGERONS 28 AND 30L AT AFT CARGO BAY. SECTION OF FRAME REMOVED IAW SRM 53-030. NEW SECTION OF FRAME, ANGLES WERE TRIMED AND DRILLED, AND PLATES WERE FABRICATED IAW SRM 53-030. INSTALLED IAW SRM 51-10-3, PAR 14, 21 AND 53-030, FIG 2A.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 69,698 hrs · 51,862 cycles

CORROSION ON FLOOR PANEL 160G. REPLACED IAW SRM 53-24-00 FIG 3 (SHEET 1,2 AND 3) AND 51-30-2.

Part: WINDOW FRAME — CRACKED (BS 1231) · airframe 63,013 hrs · 47,098 cycles

CRACK ON UPPER AFTER CORNER OF LT WINDOW RING PAN BS 1231 AT PAX CABIN. REPAIR FABRICATED IAW SRM 53-05, FIG 122. REPAIR INSTALLED IAW SRM 53-05, FIG 122 AND ER/AS 487747-14MA, 493648-14MA REV ORIG.

Part: TAB — DAMAGED (RUDDER) · airframe 63,013 hrs · 47,098 cycles

NON ROUTINE CHECK, METALLIZED AND DAMAGE POINT OF LOWER RUDDER FAIRING TAB AT RUDDER 6508A. REPAIRED IAW SRM 51-70-1AD.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 63,013 hrs · 47,098 cycles

CORROSION ON BARREL NUT HOLES 10,14 AND 25 AT HORIZONTAL STABILIZER RT OUTER JOIN UPPER SKIN XH=27.234. REPAIRED IAW SRM 55-03, PAR 30.

Part: FRAME — CORRODED (BS 1287) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON FRAME BS 1287 AND LONGERON 29R IN AFT CARGO BAY. REPAIRED IAW SRM 51-10-3, PAR 26. 53-03D FIG 2A.

Part: NUT — CORRODED (INTERCOSTAL) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

NON ROUTINE CHECK, , RUSTED NUTS OF INTERCOSTAL FROM BS 776 - 788 BETWEEN LONGERON'S 27 - 28L. NUT WAS REPLACED IAW SRM 51-30-2.

Part: ATTACH FITTING — CORRODED (NR 1 SLAT LT) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION FOUND ON FWD AND AFT BORES ON MID ATTACH FITTING OF LT SLAT PANEL NR 1 LT. REPAIRED IAW SRM 57-02, PAR 9 C(2.

Part: WINDOW FRAME — CRACKED (BS 712) · airframe 63,013 hrs · 47,098 cycles

CRACK ON LOWER AFT CORNER OF LT RING PAN WINDOW BS 712 AT PAX CABIN STRUCTURE. DAMAGE REMOVED IAW SRM 51-30-2, 51-30-3, AND 53-05, FIG 122. REPAIR FABRICATED IAW SRM 53-05, FIG 122. REPAIR INSTALLED IAW SRM 53-05, FIG 122, AND ER/A'S 487747-14MA, 493648-14MA.

Part: ATTACH FITTING — CORRODED (NR 3 SLAT LT) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

NON ROUTINE CHECK, CORROSION FOUND ON FWD AND AFT BORES ON OTBD ATTACH FITTING, ALSO FWD BORE INBD FITTING OF SLAT PANEL NR 3LT. REPAIRED IAW SRM 57-02, PAR 9, TABLE 1.

Part: ATTACH FITTING — CORRODED (NR 4 SLAT LT) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION FOUND ON FWD BORES AT MID AND INBD ATTACH FITTINGS OF SLAT PANEL NR 4 LT. REPAIRED IAW SRM 57-02, PAR A TABLE 1.

Part: FITTING — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION FOUND ON FWD BORE AT MID ATTACH FITTING OF SLAT PANEL NR 5 LT, XOS 530. CORRODED BORE AT MID ATTACH FITTING AND REPAIRED IAW SRM 57-02, PAR 9 TABLE 1.

Part: CUSP WEB — CORRODED (BS 894-901) · corrosion level 2 · airframe 63,013 hrs · 47,098 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER RT CUSP WEB BETWEEN BS 894 - 901 RBL 55 AND 60. REPAIRED IAW SRM 51-30-5, 51-10-3, & 53-0.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 69,698 hrs · 51,862 cycles

THE CARGO TRACK BS 1212 - 1322 CORRODED. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: DOOR FRAME — CORRODED (BS 636-639) · airframe 63,013 hrs · 47,098 cycles

NON ROUTINE CHECK, CORROSION FOUND ON LOWER CARGO BAY DOOR FRAME BEAM BETWEEN BS 636 TO 639. CORROSION REMOVED IAW SRM 51-10-3, PAR 26. PREVIOUS REPAIR REMOVED IAW SRM 51-30-5. FOUND WITHIN LIMITS IAW SRM 51-10-3 PAR 14 AND 21,38.

Part: CUSP WEB — CORRODED (BS 503-520) · corrosion level 2 · airframe 69,698 hrs · 51,862 cycles

CORROSION ON LH CUSP WEB BS 503 - 520 FROM X 54 - X 60. REPAIRED IAW SRM 53-05 FIG 131A AND 51-30-2 AND 51-10-3.

Part: WINDOW FRAME — SCRATCHED (BS 769-788) · airframe 63,013 hrs · 47,098 cycles

NON-ROUTINE CHECK, SCRATCHES FOUND ON WINDOW FRAME BETWEEN BS 769-788, RT AFT SIDE. REWORKED, FOUND WITHIN OF LIMITS IAW ON DAMAGE "B", ER/A 521192-14, REV ORIGINAL.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 63,013 hrs · 47,098 cycles

NON ROUTINE CHECK, REPORTED LIGHTNING STRIKES ON WINDOW BELT ON FWD LOWER CORNER BETWEEN BS 788 AND 807 LT SIDE. REPAIRED IAW ER/A 521186-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 375) · airframe 63,013 hrs · 47,098 cycles

NON-ROUTINE CHECK, CRACK ON FUSELAGE SKIN BS 375 AND LONGERON 20R FWD UPPER CORNER OF FWD CARGO BAY DOOR CUT OUT. REPAIRED IAW SRM 53-05, FIG 105.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,762 hrs · 46,935 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 31 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,663 hrs · 46,861 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT IN THE CEILING OVER THE FIRST CLASS SECTION FAILED. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,663 hrs · 46,861 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 12 - 14 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,129 hrs · 45,737 cycles

ON MX WALK AROUND, FOUND EVIDENCE OF CORROSION BLISTERS AROUND NR 1 FWD R/A ANTENNA. REPAIRED IAW ER/A 513939-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1407) · airframe 60,533 hrs · 45,330 cycles

DURING PSV AT MSP, A SKIN CRACK MEASURING 2.5"L WAS FOUND AT STA 1407, NEAR L2L. SECTION I OF ER/A 510743-14AD HAS BEEN COMPLETED. FOLLOW UP ACTION IS REQUIRED ACCOMPLISH ER/A 510743-14AD SECTION II NOT TO EXCEED 12 MONTHS FROM REPAIR ACCOMPLISHMENT. ASSOCIATED ER/A 88-510743 ADDED FOR AC 0961. MONITOR/QC SUPPORTING DATA MASK BELOW. OPEN DEFRL AUTHORITY AMM: TRM/SRM: AA: ER TOPP: REF 88-510743. COMPLETED.

Part: SKIN — CRACKED (BS 1407) · airframe 60,538 hrs · 45,332 cycles

SKIN CRACK AT BS 1407, BETWEEN LONGERON 1 AND 2L UNDER THE SKATE ANGLE. CRACKED 9-0-LT INNER SKATE ANGLE STA 1407. SUMMARY OF NRC 177: REPAIRED IAW ER/A 510743-14AD REV ORIGINAL BY INSTALLATION OF FILLER AND DOUBLER. ALL WORK ACCOMPLISHED ON PRI 510743-14 REV0,REV1, AND REV2 COINCIDES WITH FINAL ER/A 510743-14AD.

Part: SILL — CORRODED (BS 1174-1200) · airframe 60,538 hrs · 45,332 cycles

CORROSION AFT CARGO DOOR SILL UNDER PREVIOUS REPAIR DOUBLER AT AREAS COMMON TO BS 1174 TO 1200. REPAIRED IAW ERA 510752-14, REV.

Part: SKIN — CRACKED (BS 1439) · airframe 60,533 hrs · 45,330 cycles

FUSELAGE/EMPANAGE-CRACKED AT FASTENER LT SIDE, BETWEEN L-2 AND L-3, STA 1439. CRACKED ENDS MARKED HFEC 06-10-01-001. (TO 83) UPDATE INFORMATION FOR LOG PAGE 0714218. THIS ENTRY AND ER/A REQUIRES AN SDR REPORT WHICH IS SELECTED ON THIS ENTRY.

Part: SKIN — CRACKED (BS 1437) · airframe 60,533 hrs · 45,330 cycles

FUSELAGE/EMPANAGE - CRACKED AT FASTENER, STA 1437 BETWEEN RT L-2 AND L-3. SUSPECT FASTENER BELOW CRACKED NEEDS HFEC WHEN REMOVED. SUBMITTED TO ENGINEERING. REF (TO 86). THIS REPAIR ALSO INCORPORATES DISCREPANCY ON (TO 173). COMPLIED WITH ER/A 510548-14 REV ORIG FILE CODE 53-31.

Part: SKIN — CRACKED (BS 1418) · airframe 60,533 hrs · 45,330 cycles

STA 1418, FUSELAGE SKIN CRACKED INSIDE PANEL 6301B RT OF CENTER HFEC CONFIRMED CRACK NDT HFEC 06-10-01-001 MARKED. CUT OUT CRACKED AREA. NEEDS HFEC FOR CONTAINMENT. HFEC IAW NDT 06-10-01-001. DAMAGE CONTAINED. INSTALLED REPAIR IAW ER/A 510703-14, REV ORIG.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 59,992 hrs · 44,933 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24 IN THE CABIN WAS INOPERATIVE. MX FOUND WIRES BROKEN LIGHT RECEPTACLE AND CONNECTOR. BOTH THE LIGHT ASSY AND THE WIRE HARNESS WERE REPLACED AND THE SYS RETURNED TO NORMAL OPERATION.

Part: BUSHING — WORN (TAILCONE) · airframe 58,680 hrs · 44,051 cycles

DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, MAINTENANCE FOUND THE TEE PIN, BUSHING, AND UPPER RIGHT CLAMP BLOCK WORN BEYOND LIMITS. THE TEE PIN BUSHINGS AND CLAMP BLOCK WERE BOTH REPLACED AND THE RII COMPLETED. FOLLOWUP FUNCTIONAL WAS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 57,624 hrs · 43,349 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED A LOOSE CONNECTION. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 56,946 hrs · 42,895 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY LIGHT ON WALL IN VENTRAL STAIRWAY INOPERATIVE. MAINTENANCE FOUND AND REPAIRED WIRE PER BOEING SWPM. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,710 hrs · 42,722 cycles

CORROSION ON SKIN AT STA 465 TO 484 FROM STR L28 TO R 29.

Part: SKIN PANEL — CRACKED (HORIZONTAL STAB) · airframe 55,564 hrs · 41,968 cycles

HORIZ STAB REAR SPAR UPPER CAP AFT SKIN INSP EA 09-460214-12, REV D, ME07, ME13, ME14 SPLICED LT UPPER SKIN PANEL ON HORIZ STAB.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 55,564 hrs · 41,968 cycles

VERTICAL STAB LT SPAR CHORD ZFS 52 DAMAGED HOLE. REPAIRED IAW ERA 488672-14.

Part: LANYARD — MISINSTALLED (EVAC SLIDE) · airframe 55,241 hrs · 41,743 cycles

DURING LINE CHECK MAINTENANCE FOUND LANYARDS ON DOOR SLIDES L1 AND L2 INSTALLED INCORRECTLY. MAINTENANCE REPOSITIONED LANYARDS TO PROPER POSITION PER AMM 25-62-00. (2010-D1374) (DLM88103209)

Part: LIGHT — INOPERATIVE (SEAT 24E) · airframe 53,386 hrs · 40,479 cycles

EXIT SIGN AT 24E MISSING. INSTALLED NEW EXIT SIGN. CHECKS OK.

Part: CUSP WEB — CORRODED (BS 833) · airframe 48,338 hrs · 37,243 cycles

EXCESSIVE EXFOLIATION CORROSION ON LT CUSP WEB AT STA 833. REPAIRED PER ERA 398191-14MA ON N/R T0083662 AT HMV-3 AT GDL.

Part: CUSP WEB — CORRODED (BS 1048-1053) · airframe 48,338 hrs · 37,243 cycles

EXFOLIATION CORROSION ON RT CUSP WEB BETWEEN STA 1048 TO 1053, TASK CARD 58-53313. REPAIRED PER ERA 398191-14MA REV ORG ON N/R T0083346 AT HMV-3 IN GDL.

Part: CUSP WEB — CORRODED (BS 849-860) · airframe 48,338 hrs · 37,243 cycles

EXFOLIATION CORROSION ON RT CUSP WEB BETWEEN STA 849-860, BELOW CUSP WEB. REPAIRED PER ERA 398191-14MA REV A ON N/R T0083346 AT HMV-3 IN GDL.

Part: ISOLATOR — CORRODED (NR 2 ENG) · airframe 48,338 hrs · 37,243 cycles

PITTING CORROSION ON RT ENGINE AFT ISOLATOR SEAT AREA OF CONE BOLT. TASK CARD 82-54300. RT ENGINE ISOLATOR AFT MOUNT R/R ON OPN 7251. REFERENCE N/R TOO84804 AT HMV-3 IN GDL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 40,306 hrs · 31,725 cycles

ON CLIMBOUT, THE A/C DID NOT PRESSURIZE AND CREW HAD A FLOW LIGHT. PERFORMED VISUAL INSPECTION OF THE A/C NO DEFECTS NOTED. CHECK OPERATION OF THE OUTFLOW VLV, OPS NORM. PERFORMED BITE OF THE AUTO PRESS CONTROLLER CHECK GOOD. PRESSURIZED A/C FROM APU AND ENGINE PNEUMATICS. ELECTED TO INOP THE A/C, AUTO SHUT-DOWN SYSTEM AS A PRECAUTION.

Part: MOTOR — UNKNOWN (TRIM SYSTEM) · airframe 40,009 hrs · 31,501 cycles

PRIMARY TRIM INTERMITTENT AT TIMES INOP. REPLACED TRIM MOTOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,397 hrs · 30,339 cycles

AFT F/A AND FWD F/A EACH HAD ONE EMERGENCY FLASHLIGHT THAT WAS NOT FLASHING THE RED LIGHT. REPLACED BATTERY ON BOTH, OPERATION NORMAL.

Part: TIRE — FAILED (MLG) · airframe 38,390 hrs · 30,333 cycles

ON TAKEOFF FROM LGA, NR 1 TIRE BLEW OUT. DAMAGED 2 HYD LINES ON GEAR STRUT, DAMAGED GEAR STRUT DOOR AND DAMAGED SPLASH DEFLECTOR. DIVERTED TO JFK. NR 2 TIRE REMAINED INFLATED. REPAIRED OR REPLACED DAMAGED PARTS.

Part: LINE — LOOSE (NR 1 ENGINE) · airframe 33,532 hrs · 26,937 cycles

ON APPROACH APPROX 1500 AGL JUST INSIDE THE OUTER MARKER NR 1 ENG ROLLED BACK TO APPROX 40 PERCENT. PACK TRIPPED. SELECTED CONTINUOUS IGNITION. ADVANCED THROTTLES AND ENGINE RECOVERED. FOUND PS4 LINE AT PRBC LOOSE, TIGHTENED AND RESAFETIED SAME, RAN ENG PER PFHB, ALL INDICATIONS AND ENG PARAMETERS NORMAL. UNABLE TO DUPLICATE. ENG OK FOR SERVICE.

Part: SLAT — MALFUNCTIONED (WING) · airframe 32,675 hrs · 26,293 cycles

AUTO SLAT FAIL MESSAGE ON T/O ROLL AT 65 KNOTS. RTO. TESTED SYSTEM PER M/M.

Part: SMOKE GOGGLES — WORN (COCKPIT) · airframe 29,931 hrs · 24,256 cycles

CAPTS SMOKE GOGGLES CANNOT BE ADJUSTED TO FIT. ALSO, STRAP WORN JUMPSEAT, SMOKE GOGGLES SEAL IS DETERIORATED. REPLACED SAME.

Part: BATTERY — DISCHARGED (AFT CABIN) · airframe 29,914 hrs · 24,245 cycles

EMERGENCY FLASHLIGHT IN AFT CABIN INOP. REPLACED EMERGENCY FLASHLIGHT.

Part: HEATER — FAILED (STATIC PORT)

FLIGHT ATTENDANTS REPORTED BURNING SMELL NEAR FIRST CLASS/ COACH DIVIDER. A/C ON APU POWER/AIR FOR 3-5 MINUTES. TURNED OFF STATIC PORT HEATERS, ODOR DIMINISHED. DEACTIVATED STATIC HEAT REMOVING 4 CANNON PLUGS AT HEATERS. FWD TO MCO AND PLACARD. SUBSEQUENTLY REPLACED THE CAPTAINS PRIMARY STATIC PORT HEATER ON LOG NR 083545003.

Part: CONTROL VALVE — LEAKING (LANDING GEAR)

ON T/O FROM PBI, THE FLT CREW REPORTED AN ODOR IN THE CABIN. ODOR DISSIPATED ON POWER REDUCTION. ODOR RETURNED AT FL250, RT PACK WAS SHUTDOWN AND THE ODOR WENT AWAY. FLIGHT DIVERTEDTO JAX. MAINTENANCE FOUND THE MAIN LANDING GEAR CONTROL VALVE LINE LEAKING AND FLUID WAS STREAKING DOWN THE SIDE OF THE FUSELAGE. TIGHTENED LINE, PERFORMED DUCT BURNOUT. REPLACED COALESCERS.

Part: TURBINE — FAILED (APU)

AFTER TRANSIT CHECK, THICK SMOKE IN CABIN WITH LT PACK RUNNING. REPLACED APU. CLEANED APU INLET ASSY. REPLACED COALESCER BAGS. PERFORMED DUCT BURNOUT. RAN PACKS, NO SMOKE OR ODORS.

Part: WIRE — SHORTED (CABIN)

ONE SECTION OF EMERGENCY LIGHTS INOP IN AFT CABIN. REPAIRED SHORTED WIRES IN AFT STAIRWELL AREA TO EXIT SIGN.

Part: SOCKET — FAILED (CABIN OVERHEAD)

BURNING/ELECT ODOR AFT GALLEY CLIMBING THROUGH 10,000 FT, NO SMOKE. FOUND FOUR BULB HOLDER SHORTED AT BULB PINS. REPLACED THE HOLDER AND BULBS, CK'S OK.

Part: SKIN — CRACKED (FUSELAGE)

LEFT AFT NOSE GEAR DOOR HAS SMALL CRACK IN DOOR HINGE CUTOUT IN FUSELAGE. FOUND DURING F-1 LETTER CHECK. REPAIRED PER SRM 53-05, FIG 62A.

Part: ARM — FAILED (LT MLG DOOR)

ON CLIMBOUT FROM IAH, MAIN GEAR DOOR OPEN MESSAGE WOULD NOT GO OUT, DIVERTED DFW. FOUND LEFT INBOARD FLAP INBOARD HINGE WITH BROKEN ARM. THE ARM WAS LODGED IN GEAR DOOR PREVENTING IT TO CLOSE FULLY. REPLACED ARM, OPERATION NORMAL.