N947ML

Part: WIRE — BROKEN (CABIN)

MLB - DURING DAILY, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BULB AND LENSE AND ROW 4. OPERATION CHECK NORMAL IAW 33-53-0. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - EMERGENCY EXIT LIGHT INOPERATIVE. MAIN ENTRY DOOR WAY. REMOVED AND REPLACED LIGHT ASSEMBLY. FUNCTIONAL CHECK GOOD DC-9 MM CHAP 33-50-0. (M)

Part: SLIDE — LOOSE (PAX DOOR)

MAIN CABIN DOOR ESCAPE SLIDE FELL OUT DUE TO JET BLAST. REINSTALLED ESCAPE SLIDE AS REQUIRED. NO DEFECTS NOTED AT THIS TIME IAW DC9 MM 25-61-0. ALL ACCOMPLISHED. (M)

Part: PROX SWITCH — DIRTY (LANDING GEAR)

LRD - FLT 902 - LANDING GEAR EXTENSION WAS NORMAL. ABOUT 700 FEET ABOVE THE RUNWAY, RT MAIN GEAR RED UNSAFE LIGHT CAME ON FOR 1-2 SECONDS, EVER 5-10 SECONDS. WENT AROUND BUT THE LEFT GEAR DOWN. UNSAFE INDICATIONS STOPPED. USED QRH PROCEDURES, RECYCLED GEAR. AFTER LOOKING IN GEAR IN PERISCOPE, WE WERE NOT CERTAIN STRIPES WERE LINED UP. WARNING DID NOT OCCUR AGAIN AFTER GEAR WAS EXTENDED SECOND TIME. RE-RACKED PROXIMITY WARNING SYSTEM CONTROL BOX AND CLEANED RT MAIN GEAR PROXIMITY SWITCH SYSTEM. SELF TEST GOOD IAW DC-9 MM 32-60-1. (M)

Part: LIGHTS — MISSING (CABIN)

DTW - FLT 626 - MISSING 2 LIGHTS IN THE EMERGENCY TRACK LIGHTING (RED ONES) BY FWD EXITS. REINSTALLED LENS AND LAMPS IN EMERGENCY TRACK LIGHTING. OPS CHECK GOOD. (M)

Part: BULB — MISSING (CABIN)

FLL - FLT 411 - MOST FORWARD EMERGENCY FLOOR LIGHT IS INOPERATIVE AND 4TH LIGHT FROM FORWARD IS MISSING. INSTALLED BULB, OPS CHECK GOOD. (M)

Part: BULBS — MISSING (CABIN)

PIE - FORWARD SECTION OF RED FLOOR TRACK LIGHTING MISSING 2 LENSES AND LAMPS. REPLACED 2 RED LENSES AND LAMPS IN FORWARD SECTION OF FLOOR TRACK LIGHTING. OPS CHECKS OK PER DC-9 MM CHAPTER 33. (M)

Part: BULB — MISSING (CABIN)

DTW - FLT 640 - FORWARD FIRST ROW OF RED EMERGENCY EXITS LIGHTS HAS BULB MISSING. INSTALLED NEW BULB, OPS CHECK GOOD. (M)

Part: RELAY — STICKING (APU)

PIT - FLT 202 - APPARENTLY THE RIGHT A/C BUS HAS AN APU RELAY STICKING WHICH WILL NOT ALLOW ANY OTHER POWER SOURCE TO POWER THE RIGHT A/C BUS. THIS OCCURS EVEN WITH THE APU SHUT DOWN. RESET CROSS-TIE RELAY. APU GEN SYSTEM INOP. TRANSFERRED DMI LOG NR 00712 IAW MEL 24-1-2 CAT C. REMOVED AND REPLACED RT AUXILIARY RELAY IAW DC-9 MM J24-20-6. PERFORMED A/C CROSS-TIE CHECK WITH ENGINES NR 1 AND NR 2 RUNNING. A/C CROSS-TIE CHECKS GOOD. OPS CHECK NORMAL IAW FCOM. CLEARED DMI NR 00712. PLACARD REMOVED AND DISPATCH NOTIFIED THROUGH MAINTENANCE CONTROL. (M)

Part: BATTERY — DISCHARGED (CABIN)

DTW - ON DAILY INSPECTION, FOUND TRACK LIGHTING NOT TESTING PROPERLY. REPLACED TRACK LIGHTING EMERGENCY BATTERY ASSEMBLY. SYSTEM TESTED NORMAL IAW DC-9 MM 33-50-00. (M)

Part: ALTIMETER — FAILED (CAPTAINS)

ACY - FLT 178 - BARO ALTIMETER IS READING 150 FEET AT FIELD ELEVATION OF 76 FEET ON CAPTAIN'S SIDE. REMOVED AND REPLACED CAPTAIN'S ALTIMETER PER MM 34-10-6. CLEARS DMI NR 00594. PER GMM CHAPTER 4, PAGE 8.1, REV 25, ITEM 2.B.1. PITOT/STATIC LEAK CHECK TO BE ACCOMPLISHED AT THE NEXT SCHEDULE 'B' CHECK. ENTERED IN CARRY-OVER LOG - CONTROL NR 0043. (X)

Part: TIRE — FAILED (LT MLG)

MYR - FLT 111 - LEFT OTBD TIRE BLEW OUT ON EXITING RUNWAY. NORMAL BRAKING, BUT BRAKES APPEARED UNUSUALLY SENSITIVE. EXITING RUNWAY SPEED ABOUT 30 KNOTS ON HIGH SPEED TAXI-WAY MYR. NR 2 MLG TIRE DUE CHANGE, DUE TO NR 1 TIRE BLOW OUT PER GMM CHAP 4, PG 7.5. REPLACED NR 1 WHEEL AND TIRE ASSY IAW DC9 MM 32-40-1. SERVICED TIRE TO 160 PSI WITH NITROGEN. NO FOD DAMAGE FOUND IN FLAP/WHEELWELL AREA OR THE ENGINE INLET AREA. INSPECTED ANTI-SKID TRANSDUCER, CONTROL VALVE, AND SYSTEM CHECKS GOOD IAW MM 32-43-0. REPLACED NR 2 WHEEL AND TIRE ASSY IAW DC-9 MM 32-40-1. SERVICED TIRE TO 160 PSI WITH NITROGEN. (X)

Part: LENS COVER — OUT OF POSITION (AIRSTAIR DOOR)

MYR - FLT 243 - STAIRWAY DOOR LIGHT CAME ON APROXIMATELY 1 HOUR INTO FLIGHT. FOUND BOTTOM STAIR LIGHT LENS INTERFERRING WITH DOOR CLOSURE. SECURED LENS COVER. STAIRS AND DOOR OPS CHECKS GOOD. (X)

Part: WARNING LIGHT — ILLUMINATED (AIRSTAIR DOOR)

MYR - FLT 1706 - STAIRWAY DOOR LIGHT CAME ON APPROXIMATELY 1 HOUR INTO FLIGHT, BUT DID EXTINGUISH PRIOR TO LANDING. (2ND OCCURRENCE). TRANSFERRED TO DMI LOG, DMI NR 00574, FORWARD AIRSTAIR DOOR LGIHT PER MEL 33-17 (CAT C). FORWARD AIRSTAIR VERIFIED CLOSED AND LOCKED. DISPATCH NOTIFIED DTW MAINTENANCE CONTROL. (X)

Part: ELEV PWR LIGHT — MALFUNCTIONED (COCKPIT)

BOS - FLT 243 - ON TAXI OUT, ELEV POWER LIGHT CAME ON PRIOR TO TEST. DURING TEST, LIGHT ON, THEN OFF, NORMAL IND. WITHIN 30 SECONDS LIGHT REAPPEARED VERY DIM, BUT INCREASED IN INTENSITY TO FULL BRIGHT. SHUT DOWN LEFT ENGINE, NORMAL IND RESTARTED LEFT, NORMAL IND. RETURNED TO GATE. TRANSFER TO DMI NR 00568 IAW MEL 27-14. (M)

Part: BULB — FAILED (CABIN)

ACY - FLT 210 - THIRD LIGHT AFT ON FLOOR LIGHTING INOPERABLE. REPLACED BULB. OPS CHECK GOOD IAW 33-50-0. (X)

Part: MIC JACK — SHORTED (COCKPIT)

MYR - FLT 182 - LOSS OF BOTH RADIOS WHILE SITTING ON END OF RUNWAY FOR TAKEOFF. AFTER TAXI BACK TO RAMP AND DURING ENGINE SHUT DOWN, RADIOS STARTED WORKING NORMALLY. INSPECTED COMM SYSTEMS AND FOUND FAULTY MIC JACK (SHORTED INTERNALLY) AT OB'S POSITION. REMOVED AND REPLACED MIC JACK SYSTEM. GROUND CHECKS GOOD ON VARIOUS FREQUENCIES IAW MM 23-20. (X)

Part: LOCKING MECH — LACK OF LUBE (COCKPIT DOOR)

ACY - FLT 196 - COCKPIT DOOR WILL NOT LOCK DURING TAXI OUT. LUBED AND CLEANED LOCKING MECHANISM. OPS CHECK GOOD OK FOR FURTHER FLIGHT. (M)

Part: ANNUNCIATOR PNL — MALFUNCTIONED (COCKPIT)

DTW - FLT 428 - STAIRWAY DOOR LIGHT CAME ON DURING FLIGHT. TROUBLESHOT SYSTEM, FOUND INTERMITTENT ANNUNCIATOR LIGHT. REMOVED AND REPLACED ANNUNCIATOR PANEL. SYSTEM OPS CHECK GOOD IAW DC9 MM CH 52-70-0. (M)

Part: WARNING LIGHT — ILLUMINATED (STAIRWAY DOOR)

DTW - FLT 428 - IN CRUISE, STAIRWAY DOOR LIGHT ILLUMINATED. THERE WAS NOT ANY ADDITIONAL NOISE BY CABIN DOOR OR ANY PRESSURIZATION CHANGES. CYCLED AIRSTAIR SEVERAL TIMES AND LIGHT WENT OUT WITH EVERY CYCLE. OPS CHECK GOOD. (M)

Part: HINGE — BROKEN (PAX DOOR)

DTW - FLT 428 - AFT ENTRY DOOR, LOWER HINGE BROKEN. REMOVED AND REPLACED LOWER HINGE, AFT ENTRY DOOR, OVBD HINGE HALF ONLY IAW DC-9 MM 52-20. (M)

Part: AIR DATA COMP — MALFUNCTIONED (E/E COMPARTMENT)

YIP - REF DME NR 00127 (MRR NR 97-01-27-003/GTIA9700147). AUTOPILOT PORPOISES IN ALL FLIGHT MODES (CLIMB, CRUISE, DESCENT, STABILIZED FLIGHT). FUNCTIONAL CHECK PERFORMED IAW DC-9 MM 22-10-0. READ WIRING TO PITCH CHANNELS. REMOVED AND REPLACED AIR DATA COMPUTER AND PERFORMED PITOT STATIC TEST IAW DC-9 MM 22-10-1. (X)

Part: AILERON TRIM — BINDING (COCKPIT)

DTW - AILERON TRIM BINDING AND POSITION INDICATOR WILL NOT CENTER. FOUND SPIRAL DRIVE PLATE ON AILERON TRIM INDICATOR TO BE BINDING AND EXCESSIVELY WORN. REPLACED IAW DC-9 MM 27-10-7. OPS CHECK GOOD. (X)

Part: WIRE — LOOSE (NLG LIGHT)

ACY - FLT 825 - NOSE GEAR GREEN LIGHT STAYS ON WITH LANDING GEAR UP. UPLATCH CHECKS OK. LANDING GEAR INDICATIONS NORMAL IN DOWN POSITION. NOSE GEAR RED LIGHT OUT IN UP POSITION AS IT SHOULD BE. REMOVED LANDING GEAR LIGHT CLUSTER. FOUND WIRE GROUNDING OUT AT NOSE GEAR LIGHT. REPOSITIONED WIRES. LIGHT AND SWITCH CHECK NORMAL IAW 32-60-1. (X)

Part: AUTOPILOT — MALFUNCTIONED (E/E COMPARTMENT)

ACY - FLT 700 - AUTOPILOT PORPOISES PLUS OR MINUS 2,000 PER MINUTE VERTICALLY IN CLIMB, CRUISE, DESCENT, IN-FLIGHT. UNUSABLE. ENTER IN DMI LOG NR 00230 PER MEL 22-1 CAT 'C' DUE 3-15-97 ID NR 120. (MRR NR GTIA9700229). REMOVED AND REPLACED AVG COMPUTERS IAW DC-9 MM CHAPTER 22-11-00. GROUND TESTS GOOD. CLEARS DMI NR 00230 MEL 22-1 AND MRR NR GTIA9700229. (X)

Part: SKIN — CORRODED (BS 270-370)

YIP - REPAIR FUSELAGE SKIN BETWEEN FS 270 - FS 370, LONGERONS 23R TO 26R PER SPIRIT EA 5330-97-004. REPAIRED FUSELAGE SKIN AT FS 270-370, LONGERONS 23R - 26R PER SPIRIT EA 5330-97-004. (X)

Part: SKIN — DAMAGED (BS 465-500)

YIP - REPAIR FUSELAGE SKIN DAMAGE AT FS 465-500, LONGERON 23R AND 24R PER SPIRIT EA 5330-97-003. FABRICATED REPAIR IAW SPIRIT EA 5330-97-003. REPAIRED FUSELAGE SKIN FS AT 465-500 PER SPIRIT EA 5330-97-003. (M)

Part: PANEL — DELAMINATED (ADF ANT MOUNT)

YIP - LEFT ADF PANEL DELAMINATED. MANUFACTURED FIXTURE TO TRANSFER HOLES. DRILLED HOLES AND COUNTERSUNK AS REQUIRED. TEST FIT AND TRIMMED ALL EDGES OF EXCESS MATERIAL. PAINTED ANTENNA. INSTALLED USING PROPER SCREWS. (X)

Part: DOUBLER — DAMAGED (CARGO DOOR)

YIP - EXTERNAL REPAIR DOUBLER ON LOWER EDGE OF CARGO DOOR, FS 928 NEEDS TO BE REMOVED. REMOVED OLD DOUBLER AND INSTALLED NEW REPAIR DOUBLER PER EA 5330-97-005. (X)

Part: SILL — CORRODED (CARGO DOOR)

YIP - FORWARD CARGO DOOR SILL LOWER - SPOTS OF CORROSION AROUND SCREW HOLES. REMOVED CORROSION AND TREATED IAW DC-9 SRM 51-10-3. (X)

Part: DOUBLER — LOOSE RIVETS (BS 937)

YIP - REMOVE RIVETS, INSTALL HI-LOCKS IN REPAIR DOUBLER FS 937 BETWEEN LONGERONS 23L AND 24L. REMOVED RIVETS IN REPAIR DOUBLER, INSTALLED HI-LOCKS IN DOUBLER PER EA 5330-97-006. (X)

Part: PANEL — DELAMINATED (ADF ANT MOUNT)

YIP - RIGHT ADF PANEL DELAMINATED. MANUFACTURED FIXTURE TO TRANSFER HOLES. DRILLED HOLES AND COUNTERSUNK AS REQUIRED. TEST FIT AND TRIMMED ALL EDGES OF EXCESS MATERIAL. PAINTED ANTENNA. INSTALLED USING PROPER HARDWARE. (X)

Part: MOUNT — DAMAGED (LEFT ENGINE)

YIP - LEFT NACELLE, ENGINE MOUNT: UPPER AFT VIBRATION ABSORBER ASSY LOOSE, STEM BENT. ALSO, SUSPECT THREADS DAMAGED. REMOVED AND REPLACED ABSORBER IAW DC-9 MM 71-20-3. THREADS IN PYLON YOKE ATTACH BOLT GOOD. (X)

Part: OXYGEN LINE — LEAKING (CABIN)

YIP - DURING FUNCTIONAL CHECK OF OXYGEN MASK DEPLOYMENT TEST, FOUND DEFECTIVE LEAKING LINE AT SUPPLY MANIFOLD (L13 OVERHEAD PANEL LOCATION). REQUIRES LEAK CHECK. SERVICEABLE LINE INSTALLED IAW DC-9 MM 35-20-2. NO LEAKS NOTED. (X)

Part: SPLICE — CRACKED (BS 229)

YIP - FORWARD BELLY COMPARTMENT, NR 22 LONGERON CORRODED AND SPLICE PLATE CRACKED AT FS 229. REPAIRED LONGERON AT FS 229 PER DC-9 SRM 53-02. (X)

Part: CONTROL CABLE — FRAYED (LT AILERON)

YIP - LEFT WING - AILERON CABLE FRAYED NEAR FAIR LEAD AT APPROXIMATELY STA XRS 353. MANUFACTURED AND INSTALLED CABLE, TENSIONED AND SAFTIED IAW DC-9 MM CHAPTER 27-10-0 PAGES 9 AND 10, AND CABLE TENSION CHART. (X)

Part: SKIN — DAMAGED (RT TE FLAP)

YIP - REPAIR ON RIGHT FLAP TRAILING EDGE AT APPROXIMATELY STATION XRS 138-156 BE REMOVED AND REPLACED WITH NEW. REMOVED AND REPLACED RIGHT FLAP TRAILING EDGE WITH NEW PART IAW DC9 SRM 57-03 PAGE 11. (M)

Part: DOUBLER — DAMAGED (BS 351)

YIP - EXTERNAL REPAIR DOUBLER FS 351 BETWEEN LONGERONS 18R AND 20R REQUIRES REWORK. REWORKED REPAIR DOUBLER AT RIGHT FUS 351 TO C/W REQUIREMENTS OF DC-9 SRM 53-04 FIG 12B (INSTALLATION OF FINGER DOUBLER AND PROPER FASTENERS). (X)

Part: BRACKET — CRACKED (LT TE FLAP)

YIP - LEFT FLAP, INBOARD ATTACH BRACKET CRACKED. (CONFIRMED WITH EDDY CURRENT.) REMOVED AND REPLACED LEFT INBOARD ATTACH BRACKET WITH NEW BRACKET IAW DC-9 MM 20-16-0 PAGE 207. (X)

Part: FAIRING — CORRODED (LT HORIZ STAB)

YIP - LEFT HORIZONTAL STABILIZER LOWER SCRAPPER FAIRING: INTERIOR BOX CHANNEL HAS SURFACE CORROSION ALONG ATTACH EDGES. REMOVED MINOR SURFACE CORROSION IAW DC-9 SRM 51-10-3. (X)

Part: TRAP PANEL — CRACKED (MLG WW)

YIP - ULTRASONIC INDICATION FROM FORWARD MOST END OF UPPER ATTACH FLANGE THROUGH FIRST ATTACH HOLE TO FORWARD END OF SECOND ATTACH HOLE OF LEFT TRAP PANEL (APPROXIMATE LENGTH, 2 INCHES). REMOVED OUTBOARD PORTION OF CRACKED FLANGE AND CORROSION IAW DC-9 SRM 57-09, PAGE 24C (SPIRIT EA 5700-97-006). CLEANED AREA, ALODINED, AND PRIMED PER DC-9 SRM 57-09. (X)

Part: RIVET — FAILED (LT HORIZ STAB)

YIP - LEFT UPPER HORIZONTAL STABILIZER FAIRING - POPPED RIVET AT AFT ATTACH AND AFT CDCC AREA CRACKED. REPAIRED CRACK AND INSTALLED EXTERNAL DOUBLER AND FILLER PER DC-9 SRM 55-01 PAGE 7, 51-30-2 AND USING MATERIAL AS PRESCRIBED IN DC-9 SRM 55-10-0, PAGE 11, FIG 7, SHEET 2. (X)

Part: CLIP — BROKEN (BS 148)

YIP - FS 148 CIRCUMFERENTIAL APPROXIMATELY 12 INCHES LEFT OF CENTER OVERHEAD, BROKEN ANGLE CLIP. MANUFACTURED REPAIR ANGLE IAW DC-9 SRM 51-10-1. INSTALLED ANGLE IAW DC-9 SRM 51-30-1. (X)

Part: BUTE DOOR — DAMAGED (LT WING)

YIP - LEFT WING, CENTER BUTE DOOR INBOARD EDGE, SKIN DAMAGED. INSTALLED NEW DOOR ASSEMBLY IAW MM 57-20-3. (X)

Part: SKIN — DAMAGED (CARGO DOOR)

YIP - AFT CARGO DOOR, DOOR HANDLE CUT OUT - SKIN DAMAGED. REPAIRED SKIN DAMAGE IAW DC-9 SRM 52-05, FIG 30. (X)

Part: BRACKETS — CRACKED (FUSELAGE)

YIP - SINGLE POINT RE-FUELING SYSTEM, BOTH MOUNTING BRACKETS CRACKED. REMOVED DAMAGED BRACKETS AND CORRODED HARDWARE. INSTALLED NEW PARTS AND HARDWARE IAW DC-9 SRM SEC 51-01, PAGE 1 AND 51-30-1. (X)

Part: SKIN — CORRODED (WS 383-531)

YIP - RIGHT WING UPPER SURFACE TRAILING EDE HAS EVIDENCE OF CORROSION AT STA XRS 383-531 'NO STEP' AREA. BLENDED OUT CORROSION AND TREATED (REF: DC-9 SRM 51-10-3) IN NO STEP AREA STA 383-531. PREPPED, PRIMED, AND PAINTED RIGHT WING UPPER SURFACE TRAILING EDGE IAW DC-9 SRM 51-10-3B. (X)

Part: SKIN — CORRODED (WS 383-581)

YIP - LEFT WING UPPER SURFACE EVIDENCE OF CORROSION IN 'NO STEP' AREA BETWEEN STA XRS 383-581 (TRAILING EDGE). CLEANED SURFACE CORROSION, TREATED AREA, AND PAINTED IAW DC-9 SRM 51-10-3. (X)

Part: MOUNT — CORRODED (CARGO DOOR)

YIP - FORWARD CARGO DOOR AFT BUNGEE MOUNT BRACKET SPOTS OF CORROSION AT BOLT HOLES. REMOVED AND TREATED CORROSION FORWARD CARGO DOOR AFT BUNGEE MOUNT BRACKET IAW DC-9 SRM 51-10-3. (M)

Part: ANGLE — CORRODED (BS 370)

YIP - FORWARD CARGO COMPARTMENT O/H STATION 370 SPOTS OF CORROSION ON LINER SUPPORT ANGLE FROM 0 TO 16 INCH LEFT OF CENTER. REMOVED CORROSION AND TREATED IAW DC-9 SRM 51-10-3. PAINTED IAW 51-10-3B. (M)

Part: CABLE — FRAYED (DOOR SLIDE)

YIP - GALLEY DOOR EVACUATION SLIDE CABLE FRAYED AT TOGGLE. REPLACED CABLE. (X)

Part: SKIN — CORRODED (LEFT WING)

YIP - LEFT WING UPPER SURFACE HAS A SPOT OF CORROSION JUST OUTBOARD OF OVERWING EXIT WALKWAY. REMOVED CORROSION ON UPPER LEFT WING SURFACE, TREATED AND PAINTED IAW DC-9 SRM 51-10-3. (X)

Part: SKIN — DENTED (BS 424-446)

YIP - FUSELAGE SKIN DENTED AT FS 424-446 AT LONGERONS 22L AND 23L. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-9 SRM 53-04, FIGURE 38. (X)

Part: DOUBLER — CORRODED (BS 211)

YIP - ATC TRANSPONDER ANTENNA INTERNAL SKIN DOUBLER AND SURROUNDING AREA (FS 211) CORRODED. CLEANED MINOR SURFACE CORROSION PER DC-9 SRM 51-10-3. PREPPED AND SEALED WITH 1435 PRC. (X)

Part: FRAME — CORRODED (BS 180)

YIP - E AND E COMPARTMENT FRAME OUTER LEG UPPER SURFACE CORRODED AT FS 180 AT LONGERON ATTACH POINTS (LONGERONS 27R, 29L, AND 30). REMOVED CORROSION FROM EFFECTIVE LONGERONS, ALODINED, AND PRIMED. (X)

Part: SUPPORT BEAM — CRACKED (CARGO COMPT)

YIP - FORWARD CARGO BARRIER SUPPORT BEAM IS CRACKED AROUND BOLT HOLE IN BEAM FLANGE. STOP DRILLED CRACK AND INSTALLED REPAIR IAW DC-9 SRM SEC 52-01 FIGURE 2 SHEET 4. (M)

Part: SKIN — CORRODED (RT WING)

YIP - RIGHT WING UPPER SURFACE PANEL NR 1430A HAS EVIDENCE OF CORROSION. REMOVED CORROSION AND TREATED AREA AS PER DC-9 SRM 51-10-3 PAGES 18 AND 19. (M)

Part: FAIRING — CRACKED (LT LE FLAP)

YIP - LEFT WING INBOARD SLAT, INBOARD TRACK FAIRING CRACKED. REPLACED DAMAGED (CRACKED) SLAT FAIRING WITH NEW PER DC-9 SRM 51-01, PAGE 1. (X)

Part: BULKHEAD — CORRODED (BS 41)

YIP - NOSE WHEELWELL, FS 41, LATERAL SUPPORT ATTACHED TO UPPER PRESSURE BULKHEAD, CORROSION AT END NEAR CIRCUMFERENTIALS. CLEANED PER DC-9 SRM 51-10-3 PAGE 19 PARAGRAPH 32. (X)

Part: SKIN — LOOSE (LT PYLON)

YIP - LEFT ENGINE PYLON TRAILING EDGE LOOSE. REMOVED DAMAGED TRAILING EDGE AND INSTALLED NEW PER DC-9 SRM SEC 5402, FIGURE 5. (X)

Part: SKIN — CORRODED (CARGO DOOR)

YIP - FORWARD CARGO DOOR EXTERIOR SPOT OF CORROSION UPPER FORWARD AREA. CLEANED AND TREATED AREA PER DC-9 SRM 51-10-3. (X)

Part: SKIN — CRACKED (LT LE SLAT)

YIP - LEFT WING, OUTBOARD SLAT - RIVETS PULLED AT CENTER TRACK FAIRING AND OUTER SKIN CRACKED. REMOVED AND REPLACED SKIN IAW DC-9 SRM 51-01, PAGE 1. (X)

Part: CHANNEL MOUNT — CRACKED (LT PYLON)

YIP - LEFT ENGINE PYLON TRAILING EDGE, CHANNEL MOUNT CRACKED AND HOLES ENLARGED. TRAILING EDGE NUTPLATES LOOSE. REMOVED DAMAGED SECTION OF CHANNEL AND REPAIRED PER DC-9 SRM SEC 54-01 PG 7. REPLACED LOOSE NUTPLATES PER SRM SEC 51-0. (X)

Part: CIRCUMFERENTIALS — CORRODED (BS 47/37)

YIP - NOSE WHEELWELL, FS 47 AND FS 37, CIRCUMFERENTIALS. FASTENERS CORRODED, MARKED. REMOVED SURFACE CORROSION IAW SRM SEC 51-10-3. (X)

Part: SWITCH — FAILED (AIRFOIL ANTI-ICE)

DTW - FLT 626 - ON DESCENT WITH AIRFOIL ANTI-ICE ON, THE SUPPLY PRESSURE HIGH LIGHT CAME ON SEVERAL TIMES AND DUCT PRESSURE WAS 60 PSI. EACH TIME IT CORRECTED ON ITS OWN. REMOVED AND REPLACED AIRFOIL ICE PROTECTION HIGH PRESSURE SWITCH. SYSTEM OPS CHECK GOOD IAW MM 30-10-5. (M)

Part: AUTO-PILOT — MALFUNCTIONED (E/E COMPT)

FLT 174 - DTW - AUTO-PILOT PORPOISES IN ALL FLIGHT MODES. CREW DISCONTINUED USE OF AUTO-PILOT. DEFERRED PITCH ACCESS COMPUTER IAW MEL 22-1 CATEGORY C, CONTROL NR 00127. (M)

Part: SMOKE DETECTOR — SOUNDED (AFT LAV)

DTW - FLT 428 - ON DESCENT, SMOKE DETECTOR IN REAR RT LAV SOUNDED. RESET RIGHT LAVATORY SMOKE DETECTOR IN ARMED POSITION IAW DC-9 MM 26-10-0. OPS CHECK NORMAL. (M)

Part: SLIDE — LOOSE (CABIN DOOR)

FLL - FOUND MAIN CABIN DOOR SLIDE PACK LOOSE. RESECURED MAIN CABIN SLIDE PACK DOOR AS REQUIRED IAW MM CH 25-61. (M)

Part: LIGHT ASSY — INOP (FWD ENTRY)

LOG PAGE 027664. FWD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPS NORMAL IAW MM 33-53. (X)

Part: WALL COVERING — CRACKED (LT LAV WALL)

DURING X-RAY INSPECTION OF AFT PRESSURE BULKHEAD VENTRAL STAIR DOOR FRAME A1.375 INCH CRACK WAS NOTED AT UPPER LEFT CORNER APPROX 6 INCH OUTBOARD OF CENTER RADIUS AT 11 O'CLOCK POSITION. DETAILED LOW FREQUENCY EDDY CURRENT AND A DETAILED VISUAL INSPECTION OF AREA REVEALED THAT CRACK WAS IN THE LAV WALL COVERING (PLASTIC). THIS WAS CONFIRMED BY PLACING THE X-RAY FILM AND THE WALL COVERING TOGETHER. THE CRACK IN THE COVERING WAS EXACTLY THE SAME AS ON THE FILM. (M)

Part: SKIN — DENTED (BAGG DOOR)

RIGHT FUSELAGE, FORWARD OF FORWARD BAGGAGE DOOR, HAS NUMEROUS MINOR DENTS. DAMAGE INSPECTION DETERMINED, UNABLE TO REPAIR AT THIS TIME. DOUGLAS INFORMED OF DAMAGE AND APPROVED RESPONSE IAW ACTION NR 310001. REPAIRS TO BE COMPLIED WITH AT NEXT C-CHECK INSPECTION. ENTERED INTO CARRY OVER. (M)

Part: DOOR FRAME — CRACKED (AFT PRESS BLKHD)

DURING X-RAY INSPECTION OF THE AFT PRESS BULKHEAD VENTRAL STAIR DOOR FRAME, A 1.375 IN CRACK WAS DISCOVERED AT THE UPPER LEFT CORNER. EVAULATED CRACK AS DESCRIBED PER SB53-137R4 PG 19 GROUP 22 COND 4. THE AIRCRAFT IS OK FOR CONTINUED SERVICE PER SB53-137R4 PAGE NR 48. VISUAL AND X-RAY INSPECTION OF THE UPPER CORNERS IS COMPLIED AT INTERVALS NOT TO EXCEED 500 LANDINGS PER PARAGRAPH 2A OF SB 53-137R4. THIS ITEM TRANSFERRED TO CARRY OVER ITEM NR 5A-53-005, PER REPAIR. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ON PREFLIGHT, SOME OF THE OVERHEAD EMERGENCY LIGHTS WERE INOP. AS PER WIRING DIAGRAM 33-51-01, ALL EMERGENCY LIGHTING IS OPERATIVE. REPLACED AFT BATTERY PACK. (M)

Part: POWER SUPPLY — INOP (CABIN)

ON DAILY, FOUND BATTERY PACK INOP (REF PREVIOUS LOG PAGE DISCREPANCY M629). REMOVED AND REPLACED BATTERY CHARGER IAW DC-9 MM CHAP 33. OP CHECKED GOOD. (M)

Part: COFFEE MAKER — FAILED (FWD GALLEY)

TRANSFERRED FROM CABIN DISCREPANCIES LOG ITEM 1 'COFFEE POT SMELLS LIKE ITS BURNING AND WARMER BUTTON IS STUCK IN THE ON POSTION.' DEFERRED COFFEE MAKER IAW MEL 25-12 DMI 5006 CATD PLACARDED. LOG PAGE 028771. REMOVED AND REPLACED COFFEE MAKER CLEARED 5006 PLACARD REMOVED. (M)

Part: COFFEE MAKER — FAILED (FWD GALLEY)

AFTER BLOCKING INTO ACY, FLIGHT ATTENDANT REPORTED A BURN SMELL COMING FROM THE AREA OF THE COFFEE MAKER. FOUND COFFEE POT WARMER BUTTON STUCK ON 'IN' POSITION. CLEANED AND FREED BUTTON, NO OTHER SMELL IN AREA. (M)

Part: FIRE LIGHT — ILLUMINATED (LT ENGINE)

LEFT ENGINE LOOP B-LOOP FAIL LIGHT ON. SYSTEM TESTS NORMAL. INSPECTED LOOPS FOUND NOTHING ABNORMAL AT THIS TIME. LOOP FAIL LIGHT NOT ILLUMINATED. (M)

Part: FIRE LOOP — FAILED (LT ENG)

'L' FIRE LOOP B ILLUMINATED IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE FIRE LOOP. OP CHECKS GOOD. (M)

Part: BATTERY PACK — DIRTY (CABIN)

BOTH COCKPIT EMERGENCY LIGHTS WILL NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SELECTED 'ON' FOR TESTING CABIN AND COCKPIT LIGHTS. CLEANED TERMINALS AT BATTERY PACK, OP CHECKED LIGHTS OK. (M)