N925DL

Part: SWITCH — FAILED (NLG) · airframe 73,563 hrs · 55,813 cycles

ON APPROACH, RECEIVED NOSE GEAR UNSAFE LIGHT DURING GEAR EXTENSION. COMPLIED WITH QRH AND NORMAL EXTENSION FOLLOWED. IAW MCC, AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE NOSE GEAR INTERLOCK SWITCH WITH POSITIVE RESULTS DURING MULTIPLE NOSE GEAR EXTENSION/RETRACTION CYCLES.

Part: CABLE — DISLODGED (SHUTOFF VALVE) · airframe 73,558 hrs · 55,809 cycles

LEFT FIRE TEE HANDLE FEELS SPONGY. FOUND CABLE GOING TO HYD SHUTOFF VALVE OFF THE PULLEY. REPOSITIONED IAW AMM 20-10. OPS CHECKED NORMAL. INSPECTED PULLEY AND GUARDS. CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 73,384 hrs · 55,676 cycles

THE CREW DECLARED AN EMERGENCY DUE TO LOSS OF CABIN PRESSURE. AN EMERGENCY DESCENT WAS MADE TO FL100 AND THE OXYGEN MASKS DEPLOYED. MAINTENANCE FOUND BOTH 1 AND 2 PRESSURE CONTROLLERS SHOWING A CONTROLLER FAULT. THE LEFT ACM LOWER CONNECTING ELBOW DUCT BOOT WAS FOUND DAMAGED AND REPLACED. THE OUTFLOW VALVE FAILED A LEAK CHECK AND WAS REPLACED. BOTH PRESSURE CONTROLLERS 1 AND 2 AND THE CABIN PRESSURE SELECTOR PANEL WERE REPLACED. A FUSELAGE LEAK CHECK AND A SINGLE PACK CONFIDENCE CHECK WERE COMPLIED WITH AND PASSED. ALL OXYGEN MASKED WHERE REPACKED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP9163226)

Part: PSU — MALFUNCTIONED · airframe 73,384 hrs · 55,676 cycles

DURING CABIN DEPRESSURIZATION EVENT, PSU PANEL DID NOT OPEN AT SEATS 10ABC, 10DE, 13ABC, 12DE, 13DE, 14DE, 15DE, 16DE, 23DE, 24DE, 25ABC, 32ABC, 35ABC, 35DE, 36AB & 36DE. RESET PSU PANELS AND PREFORMED MANUAL EJECT OF OXYGEN MASKS, ALL SEATS AND LAVS PASSED IAW AMM 35-20-00. REQUIRES ANEROID TEST ALL GENERATOR. PREFORMED ANEROID TEST. PREFORMED ANEROID TEST.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,482 hrs · 54,986 cycles

DURING SERVICE CHECK FOUND EMERGENCY LIGHTS AT CEILING ROW 13-15 INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES. OPS CHECK NORMAL. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,869 hrs · 54,545 cycles

THE CREW FOUND THE AFT LT AND RT OVERWING EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BATTERIES AND THE LIGHTS CHECKED OK.

Part: GIRT BAR — DETACHED (ESCAPE SLIDE) · airframe 71,315 hrs · 54,148 cycles

DURING A FORCASTED SLIDE DEPOYMENT, CVG MAINTENANCE FOUND THAT THE L1 DOOR EMERGENCY ESCAPE SLIDE DID NOT DEPLOY DUE TO THE VELCRO TABS AT THE GIRT BAR BEING UN-ATTACHED. A NEW SLIDE WAS INSTALLED AT POSITION L1; REF LOG SHEET 2305013.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 70,318 hrs · 53,394 cycles

ENTRANCE DOOR FLOOR SUPPORT FRAME, SIX INCHES FROM DOOR SILL HAS CORROSION. REPLACED THE FLOOR SUPPORT IAW DWG 9936534.

Part: SUPPORT ANGLE — CORRODED (BS 1166) · airframe 70,311 hrs · 53,388 cycles

CORROSION AT CARGO TRACK SUPPORT ANGLE, BS 1166, TASK 53-139-05. REMOVED AND INSTALLED NEW ZEE CHANNEL IAW SRM 51-01, PARA 4.

Part: OVEN — SMOKE (GALLEY) · airframe 67,358 hrs · 51,252 cycles

WHILE ENROUTE, THE F/A REPORTED SMOKE FROM FIRST CLASS GALLEY OVEN. OVEN WAS TURNED OFF AND THE CIRCUIT BREAKERS WERE PULLED. THE F/A DISCHARGED A HALON FIRE EXTINGUISHER INTO THE OVEN. SMOKE DISSIPATED AND FLIGHT CONTINUED. REPLACED OVEN.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 67,303 hrs · 51,216 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTING WAS INOPERATIVE AT 27DE. MAINTENANCE REPLACED THE HARNESS AT SEAT 27DE AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 66,295 hrs · 50,541 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 27 IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE IN THE CONNECTOR, REPAIRED THE CONNECTOR PIN, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,384 hrs · 49,889 cycles

RT HORIZONTAL STABILIZER L/E INBD CLOSURE RIB WAS FOUND TO HAVE A CRACK EIGHT INCHES FORWARD OF THE THERMAL ANTI-ICE DUCT. THE CLOSURE RIB WAS REPLACED.

Part: LONGERON — CRACKED (BS 1193) · airframe 65,458 hrs · 49,943 cycles

LFEC SHOWS INTERNAL CRACK AT BS 1193, LONGERON 3RT. ACCOMPLISHED HFEC INSPECTION IAW NDT 06-10-01.001 NO CRACKS FOUND. REPAIRED IAW ER/A 517907-14AD, REV O.

Part: INLET — CRACKED (RAM AIR) · airframe 65,384 hrs · 49,889 cycles

DURING SCHEDULED HEAVY MAINTENANCE, A ONE INCH LONG CRACK WAS FOUND AT THE VERTICAL STABILIZER RAM AIR INLET DUCT RT AFT CORNER. REPAIRED IAW ER/A 517896-14.

Part: RECEPTACLE — WORN (TAILCONE RELEASE) · airframe 65,384 hrs · 49,889 cycles

MX DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYS GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED IAW SRM 51-30 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,384 hrs · 49,889 cycles

DURING LINE CHECK, MX FOUND THEY HAD NO CONTROL OF THE EMERGENCY ESCAPE LIGHTING AT THE OVERWING EXITS IN THE CABIN, WOULD NOT TURN OFF. MX REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE LIGHTS RETURNED TO A CONTROLLABLE CONDITION. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,904 hrs · 49,519 cycles

DURING LINE CHECK, MX FOUND THAT THE LT WING EXTERIOR EMERGENCY LIGHT WAS MALFUNCTIONING IN THAT IT WOULD REMAIN ON AFTER SELECTOR WAS CHANGED TO "ARMED". MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: LANYARD — MISINSTALLED (ESCAPE SLIDE) · airframe 63,404 hrs · 48,456 cycles

TAILCONE SLIDE DEPLOYMENT LANYARD WAS NOT LOOPED AROUND THE TAILCONE RELEASE MECHANISM CAM. DISCONNECTED THE LANYARD FROM CLEVIS AT THE SLIDE BOX AND RECONNECTED THE TAILCONE SLIDE DEPLOYMENT LANYARD IAW AMM 25-62-01-201. INSPECTION OF LANYARD INSTALLATION WAS COMPLIED WITH (RII).

Part: PIN — WORN (TAILCONE) · airframe 62,376 hrs · 47,749 cycles

DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM OPS 6908, MAINTENANCE FOUND THE TEE PIN, BUSHING, AND CABLE WORN BEYOND THE TEE PIN 11, CAM ASSEMBLY, AND CABLE WERE ALL REPLACED AND THE RII COMPLETED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,806 hrs · 47,413 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FORWARD OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,791 hrs · 47,402 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=773 BTW LONGERON 27 TO 28RT. FUSELAGE SKIN WAS BLENDED AND DOUBLER INSTALLED PER REPAIR IAW MD88 SRM 53-04D PARA 57.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 61,787 hrs · 47,400 cycles

CORROSION ON RT GEAR SUPPORT FITTING BUSHING BORE I/B SIDE AND NICKS ON LOWER AND UPPER SURFACE, ALSO WEAR ON VERTICAL WALL. REPAIRED PER ERA 500108-14AD ORIG REV.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON AFT UPPER CORNER IN STA Y=769 AND 750 FUSELAGE SKIN WINDOW BELT FRAME_RT. REPAIRED PER ERA 500111-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV THREE CRACKS WERE FOUND ON FUSELAGE SKIN AT THE UPPER FWD DOOR JAMB CORNER AND BTW LONGERON 20 AND 21RT OF THE FWD CARGO COMPARTMENT:0.125"LENGTH;0.437" LENGTH AND 0.468 LENGTH. FUSELAGE SKIN WAS REPAIRED IAW ERA 500104-14AD ORIG.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

SCRATCHES ON FUSELAGE SKIN UPPER FORWARD CORNER OF THE WINDOW BELT PANEL BTW STA Y=693 AND Y=712. REPAIRED PER ERA 500106-14 REV ORIG.

Part: FASTENER — MISSING (VERTICAL STAB) · airframe 61,787 hrs · 47,400 cycles

DURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABILIZER LEADING EDGE. LEADING EDGE SKIN/SPLICE WAS REPAIRED IAW ERA 500113-14AD REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

LIGHTNING STRIKES ON FWD /AFT EDGE OF WINDOW BELT FRAME BTW STA Y=427 AND 446, 465 AND 484, 541 AND 560 AT FUSELAGE SKIN. REPAIRED PER ERA 500106-14 REV ORIG.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON FWD LOWER CORNER AND AFT EDGE OF WINDOW BELT FRAME BTW STA Y=731-750 RT. SUPPLEMENT TO N/R T0237100 WITH CORRECTIVE ACTION REPAIRED PER ERA 500111-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=998-1041 BETWEEN LONGERONS 18-17LT. REF MD88 SRM 53-04D FIG 53 FOR REPAIR. FUSELAGE SKIN WAS BLENDED OUT AND WITH LIMITS REF MD88 M 53-04D PARA 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1043 AND Y=1060-1068 BTW LONGERON 18-19LT REF MD88 SRM 53-04D FIG 53. FUSELAGE WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-0 4D PARA 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1084-1089 ON L29L, Y=1124-1133 BTW LONGERON 23-26L, Y=1115 BTW LONGERON 20-21L AND Y=1105 BTW LONGERON 19-20L REF MD88 SRM 53-04D FIG 53 FOR REPAIR. FUSELAGE SKIN WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-04D PARA 57.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=1103-1110 LONGERON 28RT REF MD88 SRM 53-04D FIG 53 FOR REPAIR. CORROSION WAS REMOVED AND ARE WITHIN LIMITS PER SRM53-04D.

Part: RUDDER — DAMAGED (VERTICAL STAB) · airframe 61,787 hrs · 47,400 cycles

DAMAGED FLAME SPRAY ON SEVERAL AREAS AT RT RUDDER SURFACE. FLAME SPRAY WAS REPAIRED IAW MD88 SRM 51-70-1AD. 0-1AD PARA 23.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV A CRACK WAS FOUND OF 0.093" ON FUSELAGE SKIN AT STA Y=1212 BTW LONGERON 1 AND 2LT. REPAIRED PER ERA 500114-14AD REV ORIG.

Part: PLATE — CORRODED (HORIZ STAB) · airframe 61,787 hrs · 47,400 cycles

HIDDEN DAMAGE; CORROSION AND SCRATCHES ON BARREL NUTS AND HOLES AT RT/LT HORIZONTAL STABILIZER UPPER PLATE AFT EDGE. HORIZONTAL STABLIZER UPPER PLATE WAS REPAIRED IAW ERA 499479-14 REV ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV CORROSION WAS FOUND BETWEEN INNER FUSELAGE SKIN AND PRODUCTION DOUBLER STA Y=575 AT MID CARGO COMPARTMENT BETWEEN LONGERON 28L AND 28R. REF ERA 483854-14 REV C FOR REPAIR. REPAIRED PER ERA 500664-14.

Part: FASTENER — MISSING (VERTICAL STAB) · airframe 61,787 hrs · 47,400 cycles

DURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABLIZER LEADING EDGE REF EA 09-470871-12.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLE AT STA Y=244 BTW LONGERON 16L TO 17L. DOUBLER WAS REPLACED IAW MD88 SRM 53-04D FIG 12B.

Part: SKIN — NICKED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV NICKS WERE FOUND ON EXTERNAL FUSELAGE SKIN ALTERNATE STATIC PORT STA Y=454 BTW LONGERON 27RT AND 28RT REF MD88 SRM 53-04D FIG 12C FOR REPAIR.

Part: PANEL — DEBONDED (RT SPOILER) · airframe 61,787 hrs · 47,400 cycles

DURING HMV DISBONDED CARBON SHEET WAS FOUND ON RT WING GROUND SPOILER PANEL OUTBD EDGE. REF MD-88 SRM 51-70-1B PARA12 FOR REPAIR.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

DURING HMV CORROSION WAS FOUND ON LOWER DOOR JAMB BEAM FROM STA Y=642-687 AT MID CARGO COMPARTMENT REF MD88 SRM 53-05 FIG 123 FOR REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,787 hrs · 47,400 cycles

CRACK EXT FUSELAGE STA 1437 BETWEEN LONGS 4RT AND 5RT DAMAGED AREA TRIMMED OUT. REPAIR DOUBLER AND FILLER WERE INSTALLED IAW DC9/MD80 SRM 53-04D FIG 27. AIR DOUBLER AND FILLER WERE INSTALLED IAW DC9/MD80 SRM 53-04D FIG 27.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,566 hrs · 46,490 cycles

FUSELAGE SKIN STA 588, L29L TO L30 CORROSION. REPAIRED IAW ERA 483854-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,969 hrs · 46,039 cycles

FUSELAGE SKIN STA 1437, L-3L CRACK. REPAIRED IAW ERA 491464-14.

Part: SKIN — CORRODED (BS 1173-1200) · airframe 59,969 hrs · 46,039 cycles

DURING PSV VISIT, MX DISCOVERED CORROSION ON THE INTERNAL DOUBLER THAT IS BELOW THE C-3 CARGO DOOR JAMB BEAM. STA 1173 TO 1200 AT L-28R. REPAIRED IAW ER/A 491641-14, REV 2.

Part: UNKNOWN — SMOKE (CABIN) · airframe 59,941 hrs · 46,017 cycles

ON THE GROUND WHEN CREW TURNED PACKS ON INITIALLY THE CABIN FILLED WITH SMOKE. MAINTENANCE PERFORMED PACK BURNOUT. APU AND TAIL COMPARTMENTS WERE INSPECTED NO TROUBLE FOUND. RAN BOTH ENGINES WITH PACKS FOR 10 MINUTES AND NO SMOKE OR SMELL WAS NOTED. AIRCRAFT OK FOR SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 59,785 hrs · 45,918 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTING INOPERATIVE AT ROWS 2 C/D AND 3 C/D. MAINTENANCE REPLACED CONNECTORS. OPERATIONS CHECK WAS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,213 hrs · 44,878 cycles

C-2 BAG BIN BELLY SKIN CORRODED STA 690 TO STA 700 LONGERON 29R TO 30. REPAIRED PER ERA 483853-14ERA (DLM88101929).

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 57,514 hrs · 44,403 cycles

MX FOUND THE EMERGENCY LIGHTS AT ROWS 31-38 TO BE INOPERATIVE. MX CLEANED THE GROUND CONNECTION AT THE FLOOR. THE LIGHTS THEN CHECKED NORMALLY AND THE ACFT WAS RETURNED TO SERVICE. ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,220 hrs · 44,229 cycles

EMERGENCY EXIT LIGHTS OVER AFT LT AND RT OVERWING EXIT DOORS INOP. REPLACED POWER SUPPLY--OPS CKS NML.

Part: CONNECTOR — BROKEN (TEMP CONTROLLER) · airframe 52,490 hrs · 41,058 cycles

TAIL COMPT TEMP HI MSG FOUND RT TEMP CONTROL VLV FULL HOT WHEN TEMP CONTROL DECREASED/MSG WENT AWAY TRIED TO WARM CBN TAIL TEMP HI MSG ON AGAIN. QRH DIRECTED HP BLEED OFF. FOUND DUCT HOSE BLOWN OFF TEMP CONTROL VLV. ALSO FOUND ELECT CONN BROKEN. REMOVED AND REPLACED TEMP CONTROLLER VALVE. OPS/LK CKS OK. ALSO FOUND TAIL COMPT TEMP SENSOR FLAPPER DOOR CLOSED CLEANED SAME. REPLACED BLOWN DUCT RAN ENG AT PWR PRESSURIZED, A/C NO LKS NOTED. OK FOR SERVICE.

Part: SKIN — CORRODED (BS 693-712 S29R) · airframe 50,400 hrs · 39,736 cycles

CORROSION IN SKIN AND CARGO DOOR SURROUND DOUBLER AT FS 693-712 NEAR L-29R. CUTOUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER.

Part: ENGINE — FAILED (NR 1) · airframe 49,019 hrs · 38,836 cycles

NR 1 ENGINE INFLIGHT SHUTDOWN. EXTENSIVE DAMAGE IN TAILPIPE AREA. REMOVED AND REPLACED NR 1 ENG PER TRANS 9T102.

Part: LINE — LOOSE (NR 1 ENGINE) · airframe 47,728 hrs · 37,950 cycles

AFTER T/O OIL QTY WENT TO 10 QTS - OIL PRESS WAS 40 PSI WITH YELLOW LIGHT QTY REDUCED GRADUALLY TO 1 QT WITH PRESS AT 36-38 PSI. SHUT ENGINE DOWN WITH 1 QT REMAINING. ENGINE WIND MILLED AT 1 QT APPROX 36 - 38 PSI FOR 12 - 15 MIN. FOUND LINE TO LOW OIL PRESSURE SWITCH LOOSE. TIGHTENED SAME, ADDED 14 QUARTS OF OIL. FOUND ADDITIONAL LINES LOOSE. RESECURED LINES AND PERFORMED LEAK CHECK ON IDLE RUN. LEAK CHECK OK 444868. VERIFIED ALL OIL LINES SECURED SAFETIED PERFORM PART POWER ENGINE RUN. NO LEAKS NOTED.

Part: SKIN — DENTED (FS220-240 L17-19) · airframe 47,421 hrs · 37,736 cycles

THE FUSELAGE SKIN WAS FOUND WITH DENTS AT FS 220-240 BETWEEN L-17L AND L-19L. THE FUSELAGE FRAME IS ALSO DENTED. THE DAMAGED SKIN AND SECTION OF FRAME WERE REMOVED AND REPAIRS WERE INSTALLED.

Part: SKIN — DENTED (BS 435-449 L20R) · airframe 47,421 hrs · 37,736 cycles

DENTS WERE FOUND IN THE FUSELAGE SKIN AT FS 435-449, L20-21R. THE DAMAGED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED.

Part: SKIN — DENTED (BS 449-541 L20R) · airframe 47,421 hrs · 37,736 cycles

DENTS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FS 499-541 BETWEEN L-19R TO L-20R. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — CORRODED (FS 759-812 L29R) · airframe 47,421 hrs · 37,736 cycles

THE FUSELAGE SKIN HAS CORROSION BETWEEN BS 759-812, AND L27R - L29R. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: FRAME — CRACKED (FS 1446) · airframe 47,421 hrs · 37,736 cycles

FOUND 2 CRACKS .8 IN FS 1446 OUTER CAP AT S5R. REPAIRED ON EA 09-062073-12 OPN 0103 SRM 53-03 FIG 30 SHEET 8.

Part: FRAME — CRACKED (FS 1446) · airframe 47,421 hrs · 37,736 cycles

FOUND .8 IN CRACK FS 1446 FRAME OUTER CAP AT S3L. REPAIRED ON EA 09-062073-12 OPN 0103 SRM 53-03 FIG 30 SHEET 8.

Part: SKIN — DAMAGED (WS 210 LT) · airframe 47,421 hrs · 37,736 cycles

LT LOWER WING SKIN ACCESS PANEL ATTACHMENT FASTENER HOLE WAS DAMAGED, OVERSIZED TO 0.346 IN. HOLE OVERSIZED AND BUSHING INSTALLED.

Part: DUCT — BLOWN (NR 2 ENGINE) · airframe 43,620 hrs · 34,986 cycles

ON TAKEOFF RIGHT ENGINE FIRE LOOPS BOTH INDICATED RT ENGINE FIRE. TRIED TO RETARD RT THROTTLE BUT HANDLE WAS STIFF. RIGHT FUEL SHUTOFF SW ALSO STIFF. PULLED FIRE HANDLE AND FIRED BOTH FIRE BOTTLES AND RETURNED TO PBI. FOUND 13 STAGE BLEED AIR DUCT TO NOSE COWL BLOWN. NO DAMAGE TO COWL. FLIGHT CANCELED. REQUIRES BOTH TELEFLEX CABLES TO BE REPLACED.

Part: PROBE — INOPERATIVE (RUDDER) · airframe 39,411 hrs · 31,977 cycles

DURING CRUISE PITOT STATIC HEAT OFF LIGHT CAME ON OAP. CHECKED OHMETER AND FOUND RUDDER LIMITER READING 0. REPLACING PITOT PROBE HEATER.

Part: SENSE LINE — CRACKED (NR 2 ENGINE) · airframe 38,164 hrs · 31,067 cycles

UNABLE TO MAKE T/O POWER AT 70 KNOTS N1 REACHED 106 PERCENT FOR FOUR SECONDS. REJECTED TAKEOFF. A/C FERRY TO ATL FOR ENG CHANGE. MTC FOUND PT7 LINE CRACKED. REPLACED NR 2 ENG PER TRANS 9T102.

Part: AUTOTHRUST SYS — MALFUNCTIONED (COCKPIT) · airframe 37,348 hrs · 30,435 cycles

ON TAKEOFF ROLL ENGAGED THROTTLES DROVE TO T/O SETTING AND CLAMPED PRIOR TO 80 KNOTS. EPRS AND EPR SET MARKS STARTED TO ROLL BACK. DISCONTINUED T/O. DURING REVERSE THRUST AND TAXI BACK ENGINES LOOKED FINE. PERFORMED ENGINE TAKEOFF POWER RUN PER PFHB. ALL INDICATIONS NORMAL FOR NR 1 AND NR 2 ENGINE. TESTED AUTO THROTTLE SYSTEM, CHECKS OK.

Part: POSITION SWITCH — FAILED (START VALVE) · airframe 36,689 hrs · 29,954 cycles

RIGHT ENG START VALVE LIGHT ILLUMINATED AT FL120. POM PROCEDURES FOLLOWED. A/C DIVERTED TO MCO. FOUND VALVE POS SWITCH FAILED IN OPEN POSITION. REPLACED VALVE AND CKD SYS PER M/M. PART BORROWED FROM TWA.

Part: DUCT — DISCONNECTED (TAIL) · airframe 33,045 hrs · 27,230 cycles

TAIL COMPT HIGH TEMP LIGHT DURING CLIMBOUT. COMPLETED CHECK LIST. LIGHT EXTINGUISHED. RETURNED TO ATL. FOUND LT PACK DUCT SEPERATED AT TURBINE OUTLET - RECONNECTED SAME

Part: SKIN — DENTED (FUSELAGE) · airframe 32,613 hrs · 26,907 cycles

THE FUSELAGE SKIN WAS FOUND DENTED AT FS 218 AND LONGERON 18L. THE DENT WAS REMOVED WITH A 6 INCH X 13 INCH CUTOUT AND REPAIRED BY ERA 334309-14. THE DAMAGE WAS FOUND AT HMV.

Part: TIRE — FAILED (RT MLG)

AT ROTATION LOUD BANG, RT ENGINE COMPRESSOR STALLS. FOUND NR 4 TIRE THREW RECAP AND PIECES OF TIRE DAMAGED 6 FAN BLADED. REPLACED FAN. RT I/B FLAP DAMAGED.

Part: SWITCH — SHORTED (COCKPIT)

FLT CREW REPORTED SMOKE AND BURNING SMELL COMING FROM OVERHEAD CONTROL PANEL. IGNITION SWITCH STUCK IN A POSITION. MTC LOWERED PANEL TO FIND INDICATION OF EXCESSIVE HEAT IN AREA OF IGNITION SWITCH. REPORTED MINOR WIRE DAMAGE. MTC VERIFIED SWITCH SHORTED AND OVERHEATED. REPLACED SWITCH.

Part: LINK — WORN (RT INBD SPOILER)

AT 20,000 FT AND 300 KTS ATTEMPED TO DEPLOY SPEEDBRAKES, AIRCRAFT_ROLLED RIGHT. SPEED BRAKE RETRACTION STOPPED ROLL. REPLACED RT INBOARD FLIGHT SPOILER LINK.

Part: JAMB — CORRODED (CARGO DOORWAY)

THE LOWER JAMB PAN OF THE C1 DOOR CUTOUT WAS FOUND CORRODED. THE SECTION OF PAN BETWEEN THE FWD AND AFT CORNERS WAS CUT AND REMOVED. A NEW SECTION OF PAN WAS SPLICED IN PER THE MD-88 SRM 53-05 FIG 44 AND DOCUMENTED PER ER/A 365399-14.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLASHLIGHT AT AFT ATTENDANTS JUMPSEAT BATTERY LOW. REPLACED FLASHLIGHT.

Part: CSD — FAILED (LT ENGINE)

ON FINAL GOT L GEN OFF AND A/C X-TIE LOCKOUT. REPLACED LT CSD AND GEN PERF ELECTICAL SYS CHK, PER PFHB. CROSS TIE OPN NORMAL.

Part: AIR DISTRIBUTION — SMOKING (CABIN)

SMOKE FILLED CABIN IN FLT, ENG A/I WAS ON, LT PACK IN MANUAL, VLV POSITION .25 MARK, TEMP 50 DEGREES. ENG A/I WAS ON FOR 5 MIN PRIOR TO SMOKE. AFTER DESC TO 11M SMOKE CLEARED, SMOKE DET IN LT AFT LAV WENT OFF. RAN PACKS WITH APU AND ENG AIR. RAN AUGMENTATION VLV CK LT AND RT SIDE PER PFHB. RAN ENG'S TO T/O PWR AND INSP FOR BLOWN DUCTS OIL LKS AND CABIN SMOKE, NO TROUBLE FOUND. ENG A/I OPERATED NML.

Part: AIR DISTR — SMOKE (CABIN)

SMOKE FILLED CABIN IN FLT ENG A/I WAS ON LT PACK IN MANUAL VALVE POSITION ON .25 MARK TEMP 60 DEGREES ENG A/I WAS ON FOR 5 MIN. PRIOR TO SMOKE. AFTER DESCENT TO 11,000 FT, SMOKE CLEARED FROM CABIN FWD LAV SMOKE DETECTOR WENT OFF. RAN PACKS WITH APU AND ENG AIR. RAN AVG VALVE CK LT AND RT PER PFHB RAN BOTH ENG TO T/O AND INSPECTED FOR BLOWN DUCTS, OIL LEAKS AND CABIN SMOKE, NO TROUBLE FOUND. ENG A/I OP NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

F/A REPORTED EMERGENCY TRACK LIGHTING OUT FROM AFT GALLEY BACK TO CABIN DOOR. REPLACED AFT BATTERY PACK AND POWER SUPPLY, OPS CHECKS GOOD.

Part: PACK — SMOKING (LEFT)

IN CRUISE FL 330 ENGINE ANTI-ICE ON, OILY SMELL ALONG WITH LT A/C HIGH TEMP LIGHT ANNUNCIATED. SWITCHED FWD LT PACK TO MCO AND PLAC PER MEL 21-00-01A. RAN PACK FOR BURN-OUT, NO SMELL NOTED.

Part: AIR DISTRIBUTION — SMOKE (CABIN)

AT 21,000 FT AND 230 KTS, FLT ATTENDANTS REPORTEDSMOKE IN CABIN. INITIATED SMOKE/FIRE PROCEDURES, SMOKE DISAPATED ON THE DESCENT SMOKE HAD ACRID SMELL. RAN PACKS WITH ENGINES FOR BURNOUT. NO SMOKE OR SMELL DETECTED.

Part: PWR SUPPLY — INOPERATIVE (EXTERIOR)

EMER LIGHTS EXTERIOR AFT AREA INOP. REPLACED PWR SUPPLY, CHECKS GOOD.

Part: CADA — MALFUNCTIONED (RIGHT)

AT V1, F/O AIRSPEED AND ALT INDICATORS FAILED AND AT LIFT OFF OVERSPEED WARNING CAME ON WITH F/S FAILURE ON BOTH SIDES. GOING TO ALT ON F/O SIDE DID NOT CHANGE OR CADC BOTH ON 1. FLIGHT RETURNED TO EWR. INSTRUMENTS RETURNED TO NORMAL AFTER LANDING. REPLACED NR 2 CADC (P/N HG28D80) (SN 88111912) AND CADC SWITCH UNIT.

Part: AIR DISTR — SMOKE (CABIN)

IMMEDIATELY AFTER T/O, THE ENTIRE CABIN FILLED WITH SMOKE. RETURNED AND LANDED ASAP. NO ANTI-ICE OR APU IN USE. REPLACED APU DUE TO OIL LEAK. PERFORMED DUCT BURNOUT, REPLACED COALESCER BAGS AND RETURNED A/C TO SERVICE.

Part: DUCT COUPLING — BLOWN (TAIL COMP)

MIA - ON CLIMBOUT, AT FL110 AMBER FLOW LIGHT ON PRESSURIZATION CONTROLLER ILLLUMINATED. UNABLE TO PRESSURIZE, DIVERTED MCO. FOUND BLOWN DUCT AT LEFT WATER SEPARATOR. REPLACED SAME, OPERATION NORMAL.