N937DL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,331 hrs · 55,793 cycles

BOTH AFT OVERWING EMERGENCY EXIT LIGHT INOP, INTERIOR. R&R EMER LIGHT BATTERY PACK AT STA 671R PER WDM 33-51-12, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,331 hrs · 55,793 cycles

ROW 14 ABC OVERHEAD EMERGENCY LIGHT INOP, LT SIDE. RELAMPED EMERGENCY LIGHT AT ROW 14ABC PER WDM 33-51. A/C OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,156 hrs · 55,654 cycles

LEFT EMERGENCY FLOOD LIGHT IS INOPERATIVE. R & R THE FLOOD LIGHT IAW AMM 33-50 , OP CHECKED GOOD.

Part: WATER HEATER — DEFECTIVE (LAVATORY) · airframe 73,580 hrs · 55,184 cycles

AFT LT LAV SMOKE DETECTOR GOING OFF. R&R 3 SMOKE DETECTORS NO HELP 609925. R&R WATER HEATER PER AMM 38-14. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS.

Part: INLET — CONTAMINATED (APU) · airframe 73,573 hrs · 55,177 cycles

ON TAXI OUT, THE AFT FLIGHT ATTENDANT REPORTED SMOKE & FUMES IN AFT CABIN. RETURNED TO GATE AND DEPLANED PASSENGERS. FOUND APU INLET CONTAMINATED WITH OIL.

Part: UNKNOWN — SMOKE (CABIN) · airframe 73,228 hrs · 54,908 cycles

AFT LEFT SMOKE DETECTOR ALARMED CLIMBING THROUGH 9000FT. IMMEDIATELY SMELLED SMOKE IN COCKPIT APPROX. 30 SEC -1MIN. SMOKE ODOR CLEARED AND ALARM STOPPED. F/A'S INSPECTED LAV BIN AND SMOKE BUT DID NOT EVER SEE SMOKE OR FIRE. INSPECTED APU INLET FOR CONTAMINATION. FOUND TO BE CLEAN AND DRY. CHECK DOWNSTREAM DUCTS OF BOTH ACM'S & ANTI ICE VALVES. NO OIL FOUND. CLEAN AND DRY. ACCOMPLISHED OPERATION OF RECIRCULATION FAN, OPS CHECKED NORMAL. OPENED BOTH ENG UPPER AND LOWER COWLS FOR INSPECTION IAW 72-00-00-280-801C3 & 801C1. PERFORMED BORRSCOPE INSPECTION BOTH ENGINES LPC AND HPC. FOUND NO EVEIDENCE OF OIL LEAKS. ALSO INSPECTED BOTH ENGINES SADDLE DUCTS, NO DEFECTS NOTED. REMOVED AND REPLACED BOTH LT & RT WATER SEPARATOR COALESER BAGS IAW AMM 21-20-02-2. COMPLETED PNEU SMOKE /ODOR TROUBLESHOOTING IAW CARD 2120-2367. LEFT ENGINE REPLACED. PNEUMATIC SYS DUCT BURNOUT IAW CARD 7100-2619. NO ABNORMALITIES NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: CONNECTOR — ARCED (WATER HEATER) · airframe 73,228 hrs · 54,908 cycles

DUE TO REPORT OF AFT LEFT LAVATORY SMOKE DETECTOR SOUNDING WITH AN ASSOCIATED SMOKE ODOR. PILOT ALSO REPORTED AN IMMEDIATE SMOKE ODOR IN COCKPIT. THE COCKPIT ODOR CLEARED APPROXIMATELY 30 SEC-1MIN LATER. NO VISIBLE SMOKE REPORTED BY PILOTS OR FLIGHT ATTENDANTS, JUST A SMOKY ODOR. NO DUCT CONTAMINATION WAS FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. THE LT ENGINE WAS ALSO REPLACED ON AS A PRECAUTION, SUSPECTING IT MIGHT POTENTIALLY BE AN ODOR SOURCE DUE TO PRIOR OIL CONSUMPTION. EXTENSIVE TROUBLESHOOTING COMPLETED AND FOUND AFT LEFT LAVATORY WATER HEATER CONNECTOR WITH EVIDENCE OF ARCING. REPLACED WATER HEATER AND CONNECTOR. POST REPAIR VERIFICATION FLIGHT ACCOMPLISHED WITH NO ISSUES NOTED.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 73,228 hrs · 54,908 cycles

DURING CLIMBOUT, AFT FA SMELLED A BURNING ODOR AND AFT LEFT LAVATORY SMOKE DETECTOR WENT OFF. NO SMOKE WAS SEEN. FUMES DISSIPATED AND ALARM DEACTIVATED. NO FUMES OR ODOR WAS DETECTED. BOROSCOPED THE RT ENGINE BLEED DUCTS, LT & RT AUG VALVE, LT & RT PRU, LT & RT FLOW CONTROL VALVES, AND CROSSFEED DUCT. NO OIL FOUND. CLEANED BELLY W/WS 48 SECT AND APU INLET IAW W/C 4900-1184. FOUND HYD TRAIL FROM LT MLG WW TO APU. TIGHTEN B-NUT ON PTU, PERFORMED DUCT BURNOUT IAW W/C 7100-2619 AND REPLACED COALESCER BAGS. PRESSURIZED ACFT TO 6.0 PSIG WITH BOTH ENGINES, NO SMOKE ODOR OR ALARMS. REPLACED THE LT AND RT AFT LAVATORY WATER HEATERS IAW AMM 38-11. CHECKED GOOD. REPLACED THE LT AND RT AFT LAVATORY SMOKE DETECTORS AND BATTERIES. RAN BOTH ENGINES TO TAKEOFF POWER, NO ODOR PRESENT. OK FOR SERVICE.

Part: APU — OIL CONSUMPTION · airframe 73,218 hrs · 54,898 cycles

SMOKE IN CABIN ON TAXI IN. FOUND APU USING OIL. REPLACED APU AND COMPLETED DUCT BURNOUT AND REPLACED COALESCER BAGS.

Part: LONGERON — CRACKED (BS 1322-1338) · airframe 73,150 hrs · 54,848 cycles

AFT CARGO BAY HAD A CRACKED LONGERON END L26R BETWEEN BS 1322 TO 1338. THE LONGERON WAS REPLACED IAW DWG 5936667 REV CD AND SRM 51-30-5.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS) · airframe 73,006 hrs · 54,750 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 16DE. FOUND THE WIRE HARNESS UNDER SEAT DISCONNECTED. CONNECTED THE WIRE HARNESS, OPS CHECKED GOOD.

Part: SKIN — CRACKED (TAILCONE) · airframe 72,906 hrs · 54,679 cycles

LOWER AFT TAIL CONE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED TAILCONE IAW CARD 5350-0177-0101.

Part: PACKING — DAMAGED (HYDRAULIC SYS) · airframe 72,197 hrs · 54,175 cycles

UNIDENTIFIED SMOKE/BURNING SMELL IN COCKPIT AND AFT CABIN ON ARRIVAL. AFT LAV SMOKE DETECTOR ACTIVATED INTERMITTENTLY. CREW VERBAL ACFT FLEW THRU YELLOW HAZE PRIOR TO ODOR EVENT. TROUBLE SHOT PER ODI CHECK LIST. FOUND HYD LEAK AT FWD ENGINE FILTER MODULE DPI. REMOVED DPI AND REPLACED PACKING PER CMM 29-10-12, PERFORMED ENGINE RUN WITH NO LEAKS PRESENT, PERFORMED APU INLET CLEANING PER CARD 4900-1184(854217) C/W CARD 2120-2367CABIN SMOKE / ODOR T/S. C/W CARD 4950-2215 MINI BURNOUT C/W 2170-4139. COALESCER R&R. OK FOR SVC. MCC NOTIFIED.

Part: HINGE FITTING — CRACKED (LT WING SLAT) · airframe 70,910 hrs · 53,213 cycles

CRACKED HINGE FITTING OF SLAT PANEL NR 3, BS XOS= 332 AL LT WING. SLAT PANEL NR 3 WAS REPLACED IAW AMM 27-80-01.

Part: LONGERON — CRACKED (BS 160) · airframe 70,910 hrs · 53,213 cycles

CRACKED LONGERON NR 2L BS 160. LONGERON 2 LT, Y=160 WAS REPAIRED IAW SRM 53-02 FIG 18 AND AIR CONDITION DUCT WAS INSTALLED IAW AMM 20-10-11.

Part: BEAM — CRACKED (PAX DOOR) · airframe 70,910 hrs · 53,213 cycles

CRACK BEYOND OF STOP DRILL ON BEAM NR 2 AFT FRAME AT PASSENGER DOOR L-1. BEAM WAS REPAIRED IAW SRM 52-05D, FIG 83.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 70,910 hrs · 53,213 cycles

CORROSION ON PREVIOUS REPAIR AND BEAM AT MID CARGO COMPARTMENT LOWER DOOR JAMB. PREVIOUS REPAIR WAS REPLACE IAW SRM 53-05, FIG 123, SHEET, 3.

Part: LONGERON — CRACKED (BS 1437) · airframe 70,910 hrs · 53,213 cycles

CRACK ON LONGERON 12 LT AND BS 1437 IN AFT ACCESSORY COMPARTMENT. LONGERON WAS REPLACED IAW DWG 5911433-85 AND DRILLED AND ADJUSTED I.A.W DC-9/MD-80 SRM 51-10-4 AND NEW SECTION LONGERON WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: CHANNEL — CRACKED (BS 941) · airframe 70,910 hrs · 53,213 cycles

CRACKED AFT DOOR JAMB CHANNEL BS 941 AND X=7 AT LT WHEEL WELL AREA. CHANNEL WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 5930584, REV.

Part: SKIN — DAMAGED (BS 276) · airframe 70,910 hrs · 53,213 cycles

LIGHTNING STRIKE ON FASTENERS AT UPPER FUSELAGE BETWEEN LONGERONS 4 AND 3 LT BS 276. LIGHTNING STRIKE ON FUSELAGE SKIN ON BS Y=276 BETWEEN LONGERONS 4-3 LT WAS REPAIRED BY PLUG IAW SRM 53-04-1, PAR 3C, 2, A, 1, A.

Part: SKIN — DAMAGED (BS 838) · airframe 70,910 hrs · 53,213 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN LONGERONS 2 AND 3 LT BS 838. LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN LONGS 2-3LT, STA Y=838 WAS REPAIRED BY PLUG IAW SRM 53-04-2 PAR 3C, 2, A,1, A.

Part: DUCT — DETACHED (A/C PACK) · airframe 70,420 hrs · 52,864 cycles

FLOW LIGHT ILLUMINATED AT 33K. PERFORMED RAPID DESCENT AND CABIN ALT QRH. REGAINED CABIN ALTITUDE CONTROL IN MANUAL AND CONTINUED TO DESTINATION. MAINTENANCE FOUND BLOWN DUCT ON RT WATER SEPARATOR. REPLACED DUCT AND PERFORMED LT & RT PACK HEALTH CHECKS WITH SATISFACTORY RESULTS. PRESSURIZATION CHECKS NORMAL.

Part: OIL SYSTEM — LEAKING (APU) · airframe 69,239 hrs · 52,075 cycles

THE FLIGHT RETURNED TO DEPARTURE FOLLOWING THE AFT LAVATORY SMOKE DETECTOR SOUNDING AND THE F/A SMELLING SMOKE. MAINTENANCE FOUND THE APU LEAKING OIL. THE APU WAS REPLACED, APU AND A PNEUMATIC SYSTEM DUCT BURNOUT WAS ACCOMPLISHED.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 69,081 hrs · 51,952 cycles

MAINTENANCE FOUND THE L1 DOOR SLIDE PARACHUTE PIN DISENGAGED. THE DOOR SLIDE WAS REPLACED.

Part: COFFEEMAKER — SPARKS (GALLEY) · airframe 67,406 hrs · 50,799 cycles

AFTER TAKEOFF THE F/A SAW A FLICKER OF LIGHT IN FIRST CLASS GALLEY COFFEEMAKER AREA, FOLLOWED BY FAINT ELECTRICAL ODOR AND SLIGHT HAZE. THE COFFEEMAKER CIRCUIT BREAKER WAS PULLED AND THE SMOKE ODOR DISSIPATED. MAINTENANCE COMPLIED WITH THE "SMOKE IN CABIN" AMDS WORKCARD 2120-2367 AND ISOLATED THE FAULT TO THE COFFEEMAKER. THE COFFEEMAKER WAS REPLACED IAW AMM 25-31-00.

Part: SPAR CAP — DAMAGED (RT WING) · airframe 65,649 hrs · 49,554 cycles

RT WING REAR SPAR, XRS 164 LOWER CAP DAMAGED. DOUBLER REPAIR INSTALLED IAW SEC 06 OF WC 5710-01110-06. SEC 05,

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 65,649 hrs · 49,554 cycles

CRACK INDICATION ON VERTICAL STABILIZER CAP L/E FASTENER HOLE RT SIDE MARKED ON RED. REPAIRED IAW ER/A 525281-14AD REVISION ORIGINAL. PERFORMED RUDDER PITOT LEAK TEST IAW AMM 34-11-00. LEAK TEST GOOD. PERFORMED RUDDER PITOT HEAT TEST IAW AMM 34-11-02. HEAT TEST GOOD. PERFORMED VOR/LOC ANTENNA TEST IAW AMM 34-51-00. ANTENNA TEST GOOD.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 65,649 hrs · 49,554 cycles

CRACK INDICATION ON LT VERTICAL STAB L/E CAP FASTENER. HOLE MARKED IN RED. REPAIRED IAW ER/A 525281-14AD, REV ORIGINAL. PERFORMED RUDDER PITOT LEAK TEST IAW AMM 34-11-00. LEAK TEST GOOD. PERFORMED RUDDER PITOT HEAT TEST IAW AMM 34-11-02. HEAT TEST GOOD. PERFORMED VOR/LOC ANTENNA TEST IAW AMM 34-51-00. ANTENNA TEST GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 62,476 hrs · 47,306 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 16D IN THE CABIN WAS INOPERATIVE. MX FOUND A BROKEN WIRE AT THE CONNECTOR AND RECONNECTED IT. THE SYS RETURNED TO NORMAL OPERATION.

Part: SKIN — DAMAGED (BS 579-598) · airframe 62,359 hrs · 47,240 cycles

LIGHTNING STRIKE ON RT WINDOW BELT AROUND FRAME FROM BS 579 TO 598. RT WINDOW BELT WAS REPAIRED IAW ER/A 509654-14, REV ORIGINAL CODE 53-31, RII COMPLETED.

Part: FRAME — CRACKED (BS 1485) · airframe 62,359 hrs · 47,240 cycles

CRACKED FRAME BS 1485. FRAME REPAIRED IAW SRM DRD 53-03D, FIG 48.

Part: SKIN — DAMAGED (BS 674-750) · airframe 62,359 hrs · 47,240 cycles

LIGHTNING STRIKES AND EROSION ON LT WINDOW BELT PANEL FRAME EDGES FROM BS 674 TO 750 IAW NRC FORM OM828A, 22, 23, 24, AND 25. LT WINDOW BELT WAS REPAIRED IAW ER/A 509650-14 REV ORIGINAL.

Part: SKIN — DAMAGED (BS 927) · airframe 62,359 hrs · 47,240 cycles

LIGHTNING STRIKE ON LT WINDOW BELT FRAME FWD EDGE AND FWD LOWER CORNER FROM BS 927. AREA WAS REPAIRED ER/A 509652-14 REV ORIGINAL AND 509655-14 REV ORIGINAL.

Part: SKIN — DAMAGED (BS 1003-1022) · airframe 62,359 hrs · 47,240 cycles

LIGHTNING STRIKE ON LT WINDOW BELT FRAME FWD UPPER CORNER STA Y=1003 TO 1022. AREA WAS REPAIRED IAW ER/A 509653-14, REV ORIG.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,359 hrs · 47,240 cycles

CRACKED LONGERON 2L BS 1418 AT AFT ACCESSORY COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1212-1278) · airframe 62,359 hrs · 47,240 cycles

CORROSION ON AFT CARGO COMPARTMENT LONGERON 23L BETWEEN BS 1212 TO 1278. SECTION OF LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, DWG 5936021, REV EH.

Part: LONGERON — CORRODED (BS 1287-1297) · airframe 62,359 hrs · 47,240 cycles

CORROSION ON LONGERON 22L BETWEEN BS 1287 TO 1297 AT AFT CARGO COMPARTMENT. SECTION OF LONGERON 22L WAS REPLACED IAW SRM 53-02, FIG 18.

Part: SEAT TRACK — CORRODED (BS 596-598) · airframe 62,359 hrs · 47,240 cycles

CORROSION ON RT SEAT TRACK X=-54 FROM STA Y=596-598 AT PAX CABIN. AREA OUT OF LIMITS, REPAIRED IAW SRM 53-05, FIG 4A.

Part: SEAT TRACK — CORRODED (BS 578-579) · airframe 62,359 hrs · 47,240 cycles

CORROSION ON LT SEAT TRACK X=54 FROM BS 578 TO 579. AREA OUT OF LIMITS. REPAIRED IAW SRM 53-05, FIG 4A.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,359 hrs · 47,240 cycles

DAMAGED METALLIZED ON LT & RT SURFACES OF RUDDER. REPAIRED IAW SRM 51-70-1 AD AND CARD 2000-8149-06,

Part: SUPPORT — CRACKED (BS 947) · airframe 62,359 hrs · 47,240 cycles

CRACK ON RT HYD HAND PUMP DISCONNECT FITTING SUPPORT BS 947 X:-24 AT FWD DOOR JAMB WHEEL WELL AREA. RT MANIFOLD SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5 EA 09-076074-03 ASSOCIATED ER/A 09-076074 ADDED FOR AC 0937.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 62,359 hrs · 47,240 cycles

INADEQUATED HOLE ON LT CUSP WEB FROM STA Y=446 TO Y=465 BETWEEN X=54 TO X=60. ALSO, CORROSION BELOW ON SAME CUSP WEB AT CABIN FLOOR STRUCTURE (CFS) REF NRC (T0 268524). DAMAGE WAS REMOVED, DOUBLER WAS FABRICATED AND INSTALLED IAW 51-30-2 AND 53-05 DD FIG 827D. REPAIR WAS IDENTIFIED IAW PS 900-5-1, NR 4.

Part: DOUBLER — CORRODED (DOOR FRAME) · airframe 62,359 hrs · 47,240 cycles

CORROSION ON MID CARGO COMPARTMENT DOOR JAMB LOWER BEAM DOUBLER FROM BS 636 TO 693. REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 123 AND ER/A 499523-14MA REV ORIG.

Part: LONGERON — DAMAGED (BS 522) · airframe 62,359 hrs · 47,240 cycles

CRACK ON LONGERON 4RT BS 522. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: CONNECTOR — FAILED (EMERGENCY LIGHT) · airframe 61,868 hrs · 46,890 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT ROW 28 IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND THE EXIT ROW CONNECTOR WAS BAD AND REPLACED IT.

Part: SKIN — CRACKED (BS 1437-L2-5L) · airframe 60,879 hrs · 46,232 cycles

LEFT CROWN FUSELAGE SKIN PANEL BS 1437, BETWEEN LONGERON 2L-5L JUST BELOW THE VERTICAL STABILIZER ATTACH ANGLE WAS FOUND TO BE CRACKED AT THREE LOCATIONS, APPROX 0.5-1.0 LONG. REPAIRS WERE ACCOMPLISHED PER ER/A 502090-14.

Part: DOUBLER — CORRODED (BS 769, L29L) · airframe 60,879 hrs · 46,232 cycles

CORROSION WAS FOUND ON RADIO ALTIMETER DOUBLER AT BS 769, L29L. DOUBLER WAS REPLACED PER MD 88 SRM 53-04.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 60,424 hrs · 45,920 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 16DE IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: WIRE — BROKEN (CABIN) · airframe 60,424 hrs · 45,920 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT A EMERGENCY PATHWAY LIGHT IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES BEHIND THE LIGHT AND RE-TERMINATED THE LIGHT ASSEMBLY. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: SKIN — CRACKED (BS 1437) · airframe 60,270 hrs · 45,814 cycles

TWO CRACKS FOUND IN SKIN AT BS 1437 BETWEEN L2-3R AND L3-4R AFT RIGHT UPPER FUSELAGE AT VERTICLE STAB. CUT OUT DAMAGE AND FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-01 FIG 4 AND ER/A502147-14 REV 0.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 59,954 hrs · 45,607 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 16-28 OF THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,754 hrs · 45,467 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROW 1C AND 13C OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE LAMPS AT EACH LOCATION AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,444 hrs · 45,230 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY PER AMM33-53. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: LANYARD — MISRIGGED (L2 DOOR SLIDE) · airframe 57,933 hrs · 44,161 cycles

DURING LINE CHECK, MX FOUND L2 DOOR LANYARD DAMAGED AND INSTALLED IMPROPERLY. MX REPLACED LANYARD ON L2 DOOR IAW AMM 25-62-00.

Part: LIGHT — INOPERATIVE (SEAT 1C) · airframe 57,781 hrs · 44,063 cycles

DURING LINE CHECK, MX FOUND PATH EMERGENCY LIGHT AT SEAT 1C INOPERATIVE. MX REPLACED LIGHT ASSY AT SEAT 1C. OPS OF LIGHT NOW CHECKS WELL.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHT) · airframe 56,311 hrs · 43,027 cycles

MX FOUND THE EMERGENCY LIGHT AT SEAT 29D TO BE INOPERATIVE. MX RECONNECTED THE HARNESS. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 56,187 hrs · 42,953 cycles

DURING MAINTENANCE CHECK FOUND EMERGENCY EXIT LIGHTS OUT FROM ROW 31-36 INOP. FOUND A QUICK DISCONNECT BETWEEN 36D AND 37D BROKEN. REPAIRED QUICK DISCONNECT. OPERATIONAL CHECK OF LIGHTS IS NOW GOOD.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 56,040 hrs · 42,849 cycles

DURING LIGHTNING STRIKE INSP FOUND DAMAGE TO 2R AND 3R WINDOW FRAMES. REPAIRED DAMAGE IAW ERA 481177-14 BLENDED OUT DAMAGE AND HFEC INSPECTED BLENDS ALSO SUBMITTED DAMAGE TO MFG, ALL GOOD FOR CONTINUE IN SERVICE IAW ERA.

Part: ENGINE — LEAKING (NR 1 INTERNAL) · airframe 52,752 hrs · 40,700 cycles

CREW REPORTS OILY SMELL/ODOR IN CABIN AFTER TAKEOFF. DISSIPATED. FOUND NR 1 ENG CREATING SMOKE AND ODOR WHILE PERFORMING OPN 5088. ENGINE CHANGE.

Part: RADOME — CRACKED (FUSELAGE) · airframe 52,418 hrs · 40,495 cycles

BIRD STRIKE ON NOSE OF RADOME. C/W BIRDSTRIKE INSPECTION PER AMM FOUND RADOME CRACKED. REPLACED RADOME PER AMM.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 50,401 hrs · 39,155 cycles

EMERGENCY LIGHTS OUT AT 2C AND 31-36 DEF FOUND BY FAA. RELAMPED 2C,NOW OPS NORMAL. FOUND CONNECTOR DISCONNECTED AT 36E. RECONNECTED AND SECURED NOW OPS NORMAL. OK FOR SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 48,751 hrs · 38,029 cycles

ATB - SMOKE IN THE CABIN ON TAKEOFF/CLIMB. POWER REDUCED. SMOKE/ODOR DISSIPATED. POWER REAPPLIED, SMOKE/ODOR RETURNED ALONG WITH AFT SMOKE DETECTOR SOUNDING. CROSSFEED VALVES CLOSED. NR 2 ENG REPLACED ON TRANS 9T102.

Part: PRESSURE SWITCH — LEAKING (APU OIL SYSTEM) · airframe 48,750 hrs · 38,027 cycles

ON PUSHBACK, APU SHUTDOWN AS CABIN FILLED WITH SMOKE. MTC IN PROGRESS ON APU AND DUCT BURNOUT. FND APU LOW OIL PRESSURE SWITCH LEAKING OIL. REPLACED SAME, NO LEAKS NOTED. WHILE PERFORMING OP 5089 APU AUTO SHUTDOWN FOR LOW OIL PRESSURE. REPLACED ECU AS PRECAUTION REMOVED AND REPLACED APU PER TRANS 9T103, C/W OPN 5089 APU /ENGINE DUC BURNOUT.

Part: SKIN — GROUND DAMAGE (BS 256) · airframe 48,019 hrs · 37,512 cycles

DURING THE VISIT, THE EXISTING REPAIR INSTALLED PER 265774-14 WAS REMOVED DUE TO ADDITIONAL DAMAGE AND A LARGER REPAIR INSTALLED PER MD88 SRM 53-04 FIGURE 12C.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

FUSELAGE SKIN REPAIR - SKIN DENTED BETWEEN STA 576-579, LONGERON 18L AND 19L. PERMANENT REPAIR INSTALLED PER SRM 53-04D, FIG 12C.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

FUSELAGE SKIN REPAIR AT STA 239, STR 30 - PERMANENT REPAIR INSTALLED PR AMX REPAIR DRAWING AMR0953566R1. APPROVED BY ERA 458452-14.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

FWD CARGO DOOR JAMB REPAIR - CORROSION ON DOOR JAMB(LOWER SIDE) OF FWD CARGO COMPARTMENT BETWEEN STA 370-427. PERMANENT REPAIR INSTALLED PER SRM 53-05D, FIG 804D.

Part: SKIN — DELAMINATED (LT WING) · airframe 47,699 hrs · 37,318 cycles

LT FORWARD CENTER BUTE DOOR EXTERNAL SKIN REPLACEMENT - SEVERAL DELAMINATED AREAS ON SKIN P/N 5919586-35 BETWEEN STA XRS=170.746-XTE=251.996. EXTERNAL SKIN WAS REPLACED IAW BACG PRODUCTION DRAWING 5919586-505 AND ERA 458462-14.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

FUSELAGE SKIN REPAIR BETWEEN STA 370 AND 389, LONGERONS 29R-30 - TWO DENTS OUT OF SRM LIMITS. DAMAGED SKIN REPAIRED PR AM REPAIR DRAWING MR0953573 R1 APPROVED BY BCAG MESSAGE NR 1-260814614-2 DATED 13DEC06.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

REPAIR TO MID CARGO DOOR JAMB CORROSION - PERMANENT REPAIR INSTALLED PER SRM 53-05D, FIG 63.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

FUSELAGE SKIN REPAIR BETWEEN STA 1193 AND 1202.5 AT LONGERON 22R/H - TWO DENTS AND A DAMAGED EXISTING REPAIR REQUIRED REPAIR. FUSELAGE SKIN WAS REPAIRED AS PERMANENT IAW AMX REPAIR DRAWING AMR0653566 R2 APPROVED BY BCAG 1-257146998-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

FUSELAGE SKIN REPAIR BETWEEN STA 229-275 AND LONGERONS 15L AND 18L - DENT AND TIME-LIMITED REPAIR. DAMAGED SKIN PORTION WAS REPLACED USING A PERMANENT SPLICE REPAIR IAW SRM 53-04D,FIG 12C, VIEW F.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

THE FUSELAGE SKIN BETWEEN STA 370 AND 389, L29R - L30 HAS TWO DENTS. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 47,699 hrs · 37,318 cycles

AN EXISTING REPAIR AT STA 1174-1202, L21L-23L, WAS FOUND DAMAGED AND TWO DENTS WERE FOUND IN THE FUSELAGE SKIN. DAMAGED SKIN WAS CUT OUT AND THE EXISTING REPAIR WAS REMOVED. A NEW REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — DENTED (BS 237 L30) · airframe 47,699 hrs · 37,318 cycles

DURING HMV, A .033 BY .312 DENT WAS FOUND AT BS 237 AND LONGERON 30. AN INTERNAL FINGER DOUBLER WAS REMADE TO EXTEND BEYOND THE DAMAGE PER ERA 458452-14 AND AMX REPAIR DWG AMR0953566, R1, DTD 11/23/06.

Part: STARTER — LOOSE (NR 2 ENGINE) · airframe 46,233 hrs · 36,281 cycles

WHEN ATTEMPT START ON RIGHT ENGINE GOT START VALVE LIGHT OPEN BUT NO ROTATION. UPON INVESTIGATION FOUND THE NR 2 STARTER NOT CONTAINED AND THE REAR COMPRESSOR DUCT DAMAGED. REPLACED STARTER. PUNCTURE IN ENG HONEY COMB JUST ABOVE START REPAIRED ENG S/N726824 PER EA 49-455079-14. FOUND ENGINE CASE DAMAGED BEHIND STARTER. REMOVED ENG PER TRANS 9T102, REINSTALLED ENG AFTER EA 49-455079-14 WAS C/W, PERFORMED CHECK PER PFHB, ALL CHECKS OK. OK FOR SERVICE.

Part: CABLE — DAMAGED (T/E FLAP) · airframe 45,358 hrs · 35,656 cycles

WHILE PERFORMING OPERATION 5603 ON THE FLAPS, A FLAP BUSSING CABLE WAS FOUND WITH THE NYCOTE COVERING CRACKED/MISSING AND THE CABLE DAMAGED OVER A 4 INCH LENGTH. REPLACED CABLE.

Part: BELLOWS — MALFUNCTIONED (NR 1 ENG FCU) · airframe 40,813 hrs · 32,389 cycles

IN CRUISE FLT LVL 350 THREE HRS INTO FLT LT ENGINE WENT TO INCREASED THRUST 209 EPR 96 PERCENT N1 EGT 553, PULLED BOTH THROTTLES IDLE RT ENG RESPONDED, LT ENGINE STAYED AT HIGH THRUST FUEL HEAT ON AND ENGINE RETURNED TO NORMAL. INSPECTED MOISTURE TRAP AND SERVICED FUEL CONTROL BELLOWS. RAN ENGINE. UNABLE TO DUPLICATE.

Part: BOWL — FAILED (HYD VALVE FILTER) · airframe 40,620 hrs · 32,271 cycles

ON CLIMBOUT LOST RIGHT HYD SYSTEM QTY AND PRESSURE. AIR TURNBACK TO IAH. FOUND LEFT INBOARD ANTISKID VALVE FILTER BOWL BROKEN. REPLACED LEFT INBOARD ANTISKID VALVE, NO OTHER LEAKS NOTED.

Part: SENSOR — INOPERATIVE (RT MLG WW) · airframe 38,637 hrs · 30,925 cycles

LANDING GEAR DOOR OPEN LIGHT ON AT FL330, STAYED ON WITH CLB TO FL350. LIGHT STAYED ON APPROX 20 MINUTES THEN WENT OUT. STAYED OUT REMAINDER OF FLT. REPLACED RIGHT MLG DOOR PROX SWITCH AND ADJUSTED PER M/M 32-60-05. GEAR DOOR INDICATION NOW TESTS NORMAL.

Part: SELECTOR SWITCH — SHORTED (COCKPIT) · airframe 36,568 hrs · 29,405 cycles

ON TAXI AC VOLT/FREQ SELECTOR SWITCH ON OVHD PANEL STARTED TO SMOKE. WHEN RIGHT SELECTED VOLTS/FREQS READ ZERO WITH ENGINE RUNNING. SELECTED LEFT SMOKE STOPPED. RTB. FOUND VOLTMETER/AMMETER SELECT SWITCH BURNED AND SHORTED. REPLACED SAME. ALL OK. ACFT OK FOR SERVICE.

Part: SELECTOR SWITCH — FAULTY (COCKPIT) · airframe 36,568 hrs · 29,405 cycles

ON TAXI OUT AFTER STARTING NR 2 ENGINE THE OVERHEAD PANEL STARTED TO SMOKE. FOUND A/C VOLT/FREQ SELECTOR SW ON OVHD PANEL BAD. REPLACED SAME, CKS GOOD.

Part: LINE — LOOSE (A/C BAY) · airframe 35,986 hrs · 28,985 cycles

ON TAKEOFF SMOKE AND FUMES IN CABIN. ALL LAV SMOKE DETECTORS WENT OFF. RAN ENGS PER MCC, NO SMOKE. C/W OPNS 5088 AND 5089 ALL CHECK GOOD. FOUND LOOSE OIL SUPPLY LINE NEAR APU OIL COOLER. SECURED SAME.

Part: ACM — LEAKING (A/C BAY) · airframe 35,345 hrs · 28,523 cycles

LEFT AFT LAV SMOKE DETECTOR ACTIVATED MOMENTARILY DURING INITIAL CLIMB. SLIGHT SMOKE SMELL, BUT NONE VISIBLE. FOUND RT ACM LEAKING OIL INTERNALLY. REPLACED ACM PER M/M.

Part: SPAR — CORRODED (NR 2 PYLON) · airframe 32,537 hrs · 26,452 cycles

THE NR 2 PYLON FRONT SPAR UPPER AND LOWER LUGS WERE OVERSIZED TO REMOVE CORROSION. THE UPPER LUG WAS OVERSIZED TO 1.3695 AND THE LOWER LUG WAS OVERSIZED TO 1.3705. ERA 396435-14 OVERSIZES THE BORE AND INSTALLS A REPAIR BUSHING. THE DAMAGE WAS FOUND AT HMV.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,537 hrs · 26,452 cycles

AFT P-DOME ATTACH ANGLE CORRODED ON FWD SIDE, STA 1338 BETWEEN LBL 0 AND LBL 10. REPAIRED PER SRM 53-03 NRC 1222 AND 1247.

Part: PUMP — INOPERATIVE (NR 1 ENGINE) · airframe 32,494 hrs · 26,417 cycles

LEFT HYD PUMP FAILED. REPLACED LEFT ENGINE HYDRAULIC PUMP.

Part: WIRE — BROKEN (1R DOOR)

RED EMERGENCY TRACK LIGHTING AT 1R INOP. FOUND WIRES TO LIGHT ASSY BROKEN. REPAIRED SAME, CHECKS GOOD.

Part: REGULATOR — OUT OF ADJUST (APU)

LT GEN ON MCO, APU WOULD NOT STAY ON LINE. ADJUSTED LEFT ENGINE GEN FREQUENCY. OPS GOOD.

Part: FUEL CONTROL — MALFUNCTIONED (NR 2 ENGINE)

TAKEOFF REJECTED AT 80 KNOTS DUE TO EPR ROLLBACK ON NR 2 ENGINE. EPR WAS MOMENTARILY STABLE AT 1.86 EPR THEN ROLLED BACK T0 1.5. REPLACED ENGINE FUEL PUMP AND CONTROL.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

ACFT WOULD NOT HOLD PRESSURIZATION ON TAKEOFF. CLIMBED TO 8,000 AUTO CONTROLLERS WERE NOT ILLUMINATED. RESEATED ALL DOORS, RAN AUG VALVE CK PER PFHB PRESSURIZED A/C. NO LEAKS FOUND.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, NR 2 CHK OF A/C 937 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP FROM SEAT 24DE TO BACK OF A/C. REPLACED BATT PACK ABOVE SEAT 37DE FOR AFFECTED TRACK LIGHTING, OPS CHK NML.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SOME EMERGENCY ESCAPE LIGHTS INOPERABLE BETWEEN ROWS 24 AND 29. REPLACED AFT FLOOR TRACK LIGHT BATTERY POWER SUPPLY. OPS CKS GOOD. FOUND SOCKET AT ROW 25 SHORTED. REPLACED SAME. CKS OK.

Part: BALLAST — SHORTED (CABIN)

FLIGHT ATTENDANTS NOTICED SMOKE ABOVE OVERHEAD ROW 31. SECURED LIGHTS AND SMOKE DISAPPEARED. FOUND BALLAST AT ROW 31ED OVERHEAD SHORTED. REMOVED BALLAST BECAUSE OF SMELL. ITEM NIS CVG. FORWARD TO MCO. NEEDS P/N 339101626.

Part: EEL WIRE — FAILED (CABIN)

DURING PRE-FLIGHT, 3 ESCAPE PATH OVERWING EXIT IDENTIFIER LIGHTS FOUND INOP. REPAIRED WIRING TO LIGHTS, OPS NORMAL.

Part: DOOR — DAMAGED (NLG)

DURING SHOP INSPECTION, THE NOSE LANDING GEAR RIGHT AFT DOOR PANEL WAS FOUND WITH DAMAGE TO FWD LOWER CORNER OF DOOR. REPAIRED PER SRM 52-05.

Part: RIB — CRACKED (NR 2 SLAT)

ON THE NR 2 SLAT 37, THE LOWER SKIN HAD TO BE REMOVED TO GAIN ACCESS TO A DAMAGED RIB. A SKIN SPLICE WAS COMPLETED PER THE SRM 57-09 TO REINSTALL THE LOWER SKIN.

Part: DOOR — WORN (MID CARGO COMPT)

AT HMV, MID CARGO DOOR EDGE WORN AT FWD AND AFT EDGES AT HOOK LOCK AREA. STRAIGHTENED EDGE AND DYE CHECKED FOR CRACKS AT FWD EDGE NO CRACKS FOUND MFG AND INSTALLED DOUBLER AT AFT EDGE PER SRM 52-05 PAGE 110A FIG 26A.

Part: SEAT TRACK — CORRODED (FS 1127-1202)

AT HMV, 3RD TRACK FROM LT SIDE IN LINE WITH FWD EDGE OF L-2 DOOR IS CORRODED. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F.

Part: DOOR JAMB — CORRODED (FWD BAG BIN)

AT HMV, FWD B/B LWR DOOR JAMB CORRODED SEVERAL PLACE. REMOVED DAMAGED AREA, GROUND AREA AT ENDS OF REPAIR FOUND TO BE WITHIN LIMITS PER SRM 53-01, INSTALLED NEW SECTION OF DOOR JAMB AND DOUBLERS PER SRM 53-05 FIG 44 (REF NR'S 482, 583, 485).

Part: SEAT TRACK — CORRODED (CABIN)

DURING HMV, FOUND SEAT TRACK CORRODED 2ND FROM LEFT SIDE FROM THE FORWARD SIDE OF THE L2 DOOR TO THE AFT SIDE OF THE L2 DOOR. REPAIRED PER SRM 53-05 FIG 4F.

Part: SEAT TRACK — CORRODED (FS 220)

AT HMV, SEAT TRACK CORRODED UNDER FWD LAV LT INBD SECTION AT APPROX FS 220. MFG AND INSTALLED REPAIR PER SRM 53-05 PAGE 10G.

Part: STRINGER — CRACKED (BS 1418)

DURING HMV, FOUND R-1 STRINGER CRACKED AT ST 1418. REPAIRED PER SRM 53-02 P1, 2 AND 3.

Part: HORIZ BEAM — CRACKED (R-1 DR FWD EDGE)

DURING HMV, FOUND R-1 DOOR HORIZONTAL BEAM CRACKED. AT FWD EDGE LWR HINGE PIVOT FITTINGS NEXT TO EXTERIOR SKIN. VISIBLE THROUGH LOWER FWD CORNER LIGHTENING HOLE. REPAIRED PER SRM 52-05.

Part: LOUVERS — CRACKED (BS1497)

DURING HMV NR CARD 62 AIR LOUVERS CRACKED AT FWD END OF 2ND AND 3RD LOUVERS O/B FROM I/B END ON SUPPORT VERTICAL LEGS RT SIDE FS CANT 1497. REPAIRED PER SRM 53-05 FIG 16.

Part: SKIN — DENTED (FS 484-503)

DENT IN FUSELAGE NEEDS TO BE CHECKED MARKED TPA 10-18-94 NR 106 AT FS 484-503, RT SIDE OF FUSELAGE. SUPPLEMENT. DENT FOUND WITHIN SRM LIMITS, DYE CHECK, NO CRACKS FOUND.

Part: SKIN — LIGHTNING STRIKE (RT ELEV)

AT HMV, FOUND RIGHT ELEVATOR OUTBOARD LOWER SKIN WITH BURN MARKS. LIGHTNING DAMAGE, AT 8 INCHES FROM TIP 4 INCHES FROM T/E. REPAIRED PER SRM 55-03.

Part: FITTING — GOUGED (NR 1 LE SLAT)

AT HMV, LT WING NR 1 L/E SLAT INBD TRACK FITTING (ON SLAT) IS GOUGED IN THE RADIUS. BLENDED GOUGE WITHIN ACCEPTABLE LIMITS PER SRM 57-02 PAGE 7, TREATED AND PAINTED.

Part: COWL — DAMAGED (NR 2 ENG)

AT HMV, NR 2 ENG LOWER AFT COWL IS DAMAGED AT FWD END. REPAIRED PER SRM 54-06.

Part: SKIN — CRACKED (NLG WW)

DURING HMV NR CARD 47, SKIN CRACKED ABOVE RT NLG AFT STRUT DOOR AFT ATTACH ARM. REPAIRED PER SRM 53-05 FIG 62.

Part: NOSE COWL — DENTED (NR 2 ENGINE)

DURING SHOP INSPECTION, NR 2 ENGINE NOSE COWL WAS REPAIRED FOR A DENT IN THE LEADING EDGE LIP. REPAIRED DENT PER SRM 54-04A.