N941ML

Part: SWITCH — INOPERATIVE (COCKPIT)

CLE - FLOOR TRACK LIGHTS DO NOT ILLUMINATE WHEN SELECTED TO 'ON' POSITION IN COCKPIT. REPLACED EMERGENCY LIGHT SWITCH IN COCKPIT. OPS CHECK GOOD. (M)

Part: CONNECTOR — LOOSE (CABIN)

DTW - CABIN EMERGENCY FLOOR LIGHTS INTERMITTENTLY OFF IN FIRST 6 ROWS. CLEANED AND RESEATED CANNON PLUGS ON BATTERY PACKS PERFORMED OPS CHECK IAW MM 33-50-00. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. (M)

Part: BULB — FAILED (COCKPIT)

MLB - CO-PILOTS EMERGENCY FLOOR LIGHTS DO NOT COME ON. RELAMPED FIRST OFFICERS EMERGENCY FLOOD LIGHTS. OPERATIONS CHECK GOOD PER DC-9 MM 33-11-2. NO OTHER DISCREPANCIES NOTED. (M)

Part: BULB — FAILED (CABIN)

DTW - ROW 8 EMERGENCY TRACK LIGHT INOPERATIVE. RELAMPED ROW 8 EMERGENCY LIGHT OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND ON 'A' CHECK, LEFT EMERGENCY OVERWING EVACUATION LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AS REQUIRED IAW DC-9 MM CHAPTER 33-53-0, OPS CHECKED NORMAL. (M)

Part: TIRE — FAILED (NR 2 MLG)

ACY - FLT 201 - NR 2 MAIN WHEEL BLEW ON LANDING. REMOVED AND REPLACED NR 2 MAIN WHEEL ASSEMBLY PER MM 32-40-1. (M)

Part: PUSHROD — OUTOF ADJUST (LT SPOILER)

MYR - FLT 1703 - WHEN DEPLOYING FLIGHT SPOILER, A/C ROLLED. FOUND LEFT OUTBOARD SPOILER CONTROL VALVE LINK, PUSHROD OUT OF ADJUSTMENT. ADJUSTED PUSHROD IAW DC-9 MM CHAPTER 27-61. OPS CHECK GOOD. RIGGED LATERAL MIXERS IAW MM 27-61. (M)

Part: FAIRING — LOOSE (FLAP/FUSELAGE)

ACY - FLT 177 - JUST PASSED DOWNWING WITH FLAPS 25 AND GEAR DOWN NOTICED A PRONOUNCED LOW FREQUENCY VIBRATION. PASSENGERS IN AFT ALSO NOTICED THIS VIBRATION UPON DEPARTING THE AIRCRAFT. FOUND INBOARD TRAILING EDGE FLAP TO FUSELAGE FAIRING ON LEFT FLAP VERY LOOSE. RE-SECURED SAME AS REQUIRED. PILOT VERIFIED THAT THE NOISE THAT THE LOOSE FAIRING MADE WHEN SHAKEN WAS IDENTICAL TO THE NOISE IN FLT, SO NO TEST FLT IS REQUIRED AND A/C OK TO CONTINUE SERVICE. (M)

Part: SOCKET — BROKEN (CABIN)

DTW - ON DAILY FOUND EMERGENCY FLOOR TRACK LIGHT INOP BY SEAT 8A, SOCKET TORN APART. TRANSFERRED TO DMI LOG IAW MEL 33-24, CAT 'C' DMI NR 00711. BOS - INSTALL NEW LIGHT BULB SOCKET AND WIRES. OPS CHECK OK IAW MM 33-53-0. THIS CLEARS DMI NR 00711. DISPATCH WAS NOTIFIED. (M)

Part: LAMP — MISSING (CABIN)

MYR - FLT 1606 - EMERGENCY LIGHT IN FLOR TRACK LIGHTING (ROW 2) OUT. REPLACED MISSING LAMP AND WHITE COER. OPS CHECK GOOD. (M)

Part: LENS — MISSING (CABIN)

MYR - FLT 1606 - RED LENS MISSING FROM EMERGENCY FLOOR LIGHTING (THIRD FROM THE FRONT). REPLACED MISSING LENSES AND BULB FOR EMERGENCY FLOOR LIGHTING. OPS CHECK GOOD. (X)

Part: TIRE — FAILED (NR 2 MLG)

EWR - FLT 1600 - NR 2 MAIN TIRE REQUIRED REPLACMENT DUE NR 1 MAIN TIRE BLOWOUT. CARRY OVER ITEM NR 2 TIRE REPLACMENT PER GTIA GMM CH 4 PG 7.5, PARA 2A2. CARRY OVER NR 0038. REPLACED NR 2 WHEEL AND TIRE ASSY IAW DC-9 MM 32-40-1 SERVICED 160 PSI WITH NITROGEN. LEAK AND OPS CHECKS GOOD. CARRY OVER NR 0038 CLEARED. (X)

Part: HINGE — BROKEN (RT MLG DOOR)

DTW - DURING COMPLIANCE WITH AD 91-22-07 (AS PER WORK CARD N-3298) THE LEFT AND RT MLG OUTBOARD DOORS AND HINGES WERE INSPECTED AND THE FOLLOWING DISCREPANCY WAS NOTED. LEFT OUTBOARD MLG DOOR UPPER HINGE, AFT LOBE CRACKED. REMOVED AND REPLACED LEFT OUTBOARD MLG DOOR IAW MM CHAPTER 32-12-1. OPS AND RIG CHECK GOOD. (M)

Part: TIRE — FAILED (MLG)

EWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. REMOVED AND REPLACED MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. REFERENCE GTIA9700247.

Part: TIRE — FAILED (MLG)

EWR - FLT 1605 - ON POST/PREFLIGHT, FOUND NR 1 MAIN TIRE BLOWN. NR 2 MAIN TIRE NEEDS REPLACED DUE TO AIRCRAFT TAXIED ON NR 1 MAIN WHEN BLOWN. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. REMOVED AND REPLACED MAIN TIRE AND WHEEL ASSEMBLY PER MM CHAPTER 32-40-1, PAGE 201. (M)

Part: PRESS SYSTEM — MALFUNCTIONED (CABIN)

BOS - FLT 248 - ON TAKEOFF, AUTO PORTION OF CABIN PRESSURIZATION DID NOT WORK. MANUAL WORKED WELL FOR REMAINDER OF FLIGHT USING FCOM PROCEDURES. DEFERRED PER MEL 21-24. MX CONTROL AUTHORIZED DMI NR 00250 CAT 'C'. (X)

Part: SWITCH — FAILED (LT SPOILER)

MDW - FLT 1704 - AFTER PUSH BACK AT MYR, SPOILER DEPLOYED LIGHT ILLUMINATED, ACCOMPLISHED PROCEDURE AS PER MEL 27-32, CONTINUED FLIGHT AS PER MEL. LIGHT EXTINGUISHED AFTER TAKEOFF AND NEVER RE-ILLUMINATED. TRANSFERRED TO DMI LOG NR 00252 IAW DC-9 MEL 27-32 CAT 'B' PLACARD INSTALLED. REMOVED AND REPLACED INBOARD AND OUTBOARD SPOILER DEPLOYED SWITCHES ON LEFT WING AND ALSO REPLACED BOTH CONNECTORS IAW DC-9 MM CHAPTER 27-60-0 THIS CLEARS DMI 00252. (M)

Part: WARNING LIGHT — ILLUMINATED (SPOILER SYSTEM)

MDW - FLT 1701 - AFTER PUSH-BACK AT MYR, SPOILER DEPLOYED, LIGHT ILLUMINATED. ACCOMPLISHED PROCEDURE PER MEL 27-32, CONTINUED FLIGHT PER MEL. LIGHT EXTINGUISHED AFTER TAKEOFF AND NEVER RE-ILLUMINATED. TRANSFERRED TO DMI LOG NR 00252 IAW DC-9 MEL 27-32 CAT 'B'. PLACARD INSTALLED. (X)

Part: WHEEL — RATTLES (NLG)

DTW - FLT 626 - NOSE WHEEL RATTLES DURING TURNS AT SLOW SPEED. REMOVED BOTH NOSE WHEEL ASSEMBLIES AND INSPECTED. NO FAULTS FOUND. RE-INSTALLED TIRE ASSEMBLIES IAW DC-9 MM 32-42. OPS CHECK GOOD. (X)

Part: TIRE — FAILED (NR 1)

ACY - FLT 700 - NR 1 MAIN TIRE EXPERIENCED A BLOW OUT. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY IAW DC9 MM CHAPTER 32. OK FOR SERVICE. (X)

Part: TIRE — FAILED (NR 2)

ACY - FLT 700 - NR 2 MAIN TIRE REQUIRES REPLACMENT DUE TO NR 1 MAIN TIRE BLOW OUT. TRANSFERRED TO CARRY OVER LOG ITEM 0019 IAW GTIA GMM CHAPTER 4, PAGE 7.5, PARAGRAPH 2.A.2. 3-1-97 - REPLACED NR 2 MAIN TIRE ASSY IAW MM CHAPTER 32-40-1. TIRE SERVICED TO 160 PSI. THIS CLEARS CARRY-OVER ITEM 0019. (X)

Part: AOA TRANSDUCER — FAILED (E/E COMPARTMENT)

DTW - FLT 428 - STALL WARNING FAILURE LIGHT COMES ON INTERMITTENTLY AND SHAKER ACTIVATES. REMOVED AND REPLACED LEFT ANGLE OF ATTACH TRANSDUCER IAW DC-9-MM 94-14-0 PAGE 210. OPS AND PREFLIGHT CHECK GOOD. (M)

Part: TRAPEZOIDAL PNL — CRACKED (RIGHT)

DURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER SERVICE BULLETIN 53-182 RIGHT TRAP PANEL CRACKED EXTENDING FROM LEADING EDGE OF PANEL TO SECOND FASTENER. EDDY CURRENT BOLT HOLE INSPECTION CONFIRMS CRACK IS ONLY FROM FIRST HOLE TO FRONT EDGE OF PANEL LENGTH 1 INCH ROUTED OUT CRACK PER S/B 53-100. (M)

Part: TRAPEZOIDAL PNL — CRACKED (LEFT)

DURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER S/B 53-182. LEFT TRAP PANEL CRACKED EXTENDED BEYOND EXISTING APPROVED SRM 57-09 FIGURE 6 SHEET 4 REPAIR IT RUNS PAST 4 FASTENER. DAC NOTIFIED ROUTED OUT CRACKED AREA .090 PAST AFT EDGE OF 4TH HOLE. EDDY CURRENT AND ULTRASOUND CONFIRM CRACK COMPLETELY REMOVED. LEFT TRAP PANEL PLACED ON WATCH WITH 400 HOUR VISUAL INSPECTION AND REPLACE AT C-CHECK BUT NOT TO EXCEED 1500 HRS. (M)

Part: DOOR LOCK — OUT OF ADJUST (RT EMER EXIT)

REF - CABIN LOG ENTRY NR 1 FROM C/N 8113 EMERGENCY EXIT HATCH ROW 15. AIRCRAFT RIGHT COMES LOOSE ON LANDING. INSPECTED AND ADJUSTED DOOR LOCK BAR IAW DC-9 MM 52-20-0. (M)

Part: CONNECTOR — LOOSE (B-FIRE LOOP)

FOUND ON DAILY, NR 1 ENGINE FIRE DETECTOR B-LOOP INOP. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DEFERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 26-1 DMI NR 002701. S/D REMOVED AND REPLACED CONNECTOR AT B-LOOP HARNESS APRON. OPS CHECK SATISFACTORY. THIS CLEARS DMI NR 2701. (M)

Part: OXY HOSE — FAILED (COCKPIT)

DURING CLIMB-OUT OF 18,000 FEET, CREW OXYGEN BOTTLE INDICATED JUST BELOW 1500 PSI. RETURNED TO DTW. SHUT OFF BOTTLE AT 1300 PSI. WITH BOTTLE OFF, OXYGEN STILL DECREASED TO 1200 PSI. REMOVED AND REPLACED CREW OXYGEN BOTTLE. FOUND CRACKED OXYGEN FITTING ON OXYGEN REGULATOR HOSE. REMOVED AND REPLACED OXYGEN HOSE ASSY. NO LEAKS OK FOR FLT. (M)

Part: CONNECTOR — INOP (B FIRE LOOP)

NR 1 ENGINE FIRE DETECTOR B-LOOP INOP, FOUND ON DAILY. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DEFERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 26-1 DMI NR 002701. (M)

Part: WIRE — DETERIORATED (RT MLG)

RIGHT LANDING GEAR UNSAFE LIGHT FLICKERS INTERMITTENTLY DURING TRANSIT OF LANDING GEAR BOTH IN RETRACTION AND EXTENSION. REPAIRED WIRING AT AND REPLACE CANNON PLUG ON RIGHT LANDING GEAR UPLIMIT SWITCH. (M)

Part: WIRE — BROKEN (LT MLG WW)

LEFT MAIN INTRANSIT RED LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. FOUND BROKEN WIRES IN LEFT MAIN WHEEL WELL, REPAIRED SAME. (M)

Part: FUEL CONTROL — OUT OF ADJUST (LT ENGINE)

LOG PAGE 7770. ABORTED TAKEOFF. ON TAKEOFF, LEFT ENGINE DEVELOPED ONLY 1.8 EPR AT 90 PERCENT N1, RIGHT ENGINE DEVELOPED 1.78 EPR AT 88 PERCENT N1, BOTH POWER LEVERS WERE AGAINST THE STOPS. CORRECTIVE ACTION: TRIMMED NR 1 AND NR 2 ENGINES IAW MM 71-00. REFERENCE TRIM CHARTS FIGURE 508. OPS CHK NORMAL. (X)

Part: PAX DOOR — WOULD NOT CLOSE (CABIN)

MAIN CABIN DOOR WOULD NOT CLOSE. CLOSED FORWARD AIR STAIR DOOR IAW DC-9MM 52-11-0. (M)

Part: FRAME — CRACKED (BS Y1104.937)

DURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104.937 BETWEEN LONGERON 10 RIGHT TO 16 RIGHT CRACKED. REPLACED FUSELAGE CANTED FRAME SECTION IAW SRM 51-01, PARAGRAPH C. (M)

Part: PANEL — CRACKED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE FLAP CENTER PANEL OUTBOARD ATTACH FITTING AT XFS187 CRACKED. REPLACED RIGHT WING TRAILING EDGE FLAP CENTER PANEL OUTBOARD ATTACH FITTING IAW SRM 51-01, PARAGRAPH C AND SRM 51-30-2 AND FAA FORM 8110-3 DATED NOV 9, 1995. (M)

Part: SPAR — CORRODED (RSS 129 LT & RT)

DURING C-CHECK, FOUND LEFT AND RIGHT WING UPPER REAR SPAR CAP FLANGES AT RIGHT STATION XRS129 AND LEFT STATION XRS127.5 CORRODED. REWORKED LEFT AND RIGHT UPPER REAR SPAR CAP FLANGES IAW MCDONNELL DOUGLAS INSTRUCTION ON FILE 95-11-06-014/AJC00146 DATED NOV 8, 1995 AND FAA FORM 8110-3 DATED NOV 10, 1995. (M)

Part: FLOOR BEAM — CORRODED (BS 965.09)

DURING C-CHECK, FOUND THE PAX/FLOOR BEAM LOWER CHORD AT STATION Y965.09 BETWEEN PLUS X6.7 TO PLUS X18 AND BETWEEN PLUS X21.5 TO PLUS 53.5 CORRODED. REPAIRED PAX/FLOOR BEAM LOWER CHORD AT IAW COOPESA DWG NO HSE9-53-140 REV A DATED NOV 12, 1995 AND FAA FORM 8110-3 DATED NOV 13, 1995. (M)

Part: SUPPORT — CRACKED (RT WING)

DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE FLAP LOWER FITTING SUPPORT AT XRS324.00 CRACKED. REPLACED RIGHT WING TRAILING EDGE FLAP LOWER FITTING SUPPORT IAW COOPESA DWG HSE9-57-242 DATED NOV 14, 1995 AND FAA FORM 8110-3 DATED NOV 14, 1995. (M)

Part: FRAME — CRACKED (BS 1104)

DURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104, LONGERON 4 LEFT CRACKED. REPAIRED FUSELAGE CANTED FRAME SECTION IAW SRM 53-01, FIG 2. (M)

Part: SKIN — CORRODED (Y1121-1136)

DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y1121 TO STATION Y1136, LONGERONS 20 RIGHT TO 21 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-01, FIG 2, PAGE 8, SRM 51-30-2. (M)

Part: FRAME — CRACKED (BS 1104)

DURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104 BETWEEN LONGERONS 10 LEFT TO 23 LEFT CRACKED. REPLACED FUSELAGE CANTED FRAME SECTION IAW ARM 51-01, PARAGRAPH C. (M)

Part: SKIN — CORRODED (BS 451-465)

DURING C-CHECK, FOUND FUSELAGE SKIN SECTION AT PITOT STATIC PORT AREA BETWEEN STATION Y451 TO STATION Y465, LONGERONS 23 LEFT TO 26 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04, FIG 31, SHEET 1. (M)

Part: FRAME — CRACKED (BS 718)

DURING C-CHECK, FOUND RIGHT CENTER OVER WHEEL FRAME, P/N 9919618-2N, AT STATION Y718, CRACKED. REPLACED RIGHT CENTER FRAME IAW MD S/B 53-131 REV 3, DATED FEB 11, 1988 OPTION 2, GROUP III, FIG 4. (M)

Part: LONGERON — CORRODED (BS 356.7-415)

DURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION BETWEEN STATION Y356.7 TO STATION Y415 CORRODED. REPLACED LONGERON 30 SECTION IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 53-02 FIG 14, DATED NOV 13, 1995 AND FAA FORM 8110-3 DATED NOV 13, 1995. (M)

Part: SUPPORT — CORRODED (BS 815)

DURING C-CHECK, FOUND AFT CARGO COMPT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y815 BETWEEN LONGERON 27 RT AND 28 RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: LONGERON — CRACKED (BS 446-465)

DURING C-CHECK, FOUND THE FUSELAGE LONGERON 25 LEFT BETWEEN STATION Y446 TO Y465 CRACKED. REPAIRED THE LONGERON 25 IAW SRM 53-02 FIG 2A. (M)

Part: LONGERON — CORRODED (BS 1109-1114)

DURING C-CHECK, FOUND FUSELAGE LONGERON 14 LEFT BETWEEN STATION Y1109 TO STATION Y1114 CORRODED. REPAIRED LONGERON 14 LEFT IAW SRM 53-02, FIG 2A. (M)

Part: SKIN — CORRODED (BS 756-775)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH LIGHT CORROSION BETWEEN Y756 AND Y775, LONGERON 26 LEFT AND LONGERON 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-04 FIG 38. (M)

Part: FITTING — CORRODED (BS 996)

DURING C-CHECK, FOUND FUSELAGE LONGERON 20 RIGHT END FITTING AT STATION Y996 CORRODED. REPLACED LONGERON 20 END FITTING IAW SRM 51-01 PARAGRAPH C AND SRM 51-10-2. (M)

Part: LONGERON — CRACKED (BS 756-802)

DURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION, P/N 592030350, IN BETWEEN STATION Y756 TO STATION Y802 CRACKED. REPLACED LONGERON 30 IAW SRM 51-01 PARA C, SRM 51-30-2. THE FRAMES AT STATION Y775 AND STATION Y794 WERE CUT FOR ACCESS AND REPAIRED IAW SRM 53-03 FIG 2A PAGE 4. (M)

Part: FLOOR BEAM — CORRODED (BS 965.09)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR BEAM Y965.09 WITH CORROSION BETWEEN XO AND PLUS X58. REPAIRED FLOOR BEAM LOWER CHORD AT Y965.09 BETWEEN PLUS X6.7 TO PLUS X 18 AND BETWEEN PLUS 21.5 TO PLUS X535 IAW EO NR COO-9-53-138-95. (M)

Part: LONGERON — CORRODED (BS 359-389)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y359 AND Y389. REPLACED LONGERON 30 FROM Y356.7 TO Y415 IAW SRM 51-01, PARA C. INSTALLED TWO SPLICES IN LONGERON 30 FROM Y 356.7 TO Y415. INSTALLED RIVETS IAW SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 980)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y980 WITH CORROSION BETWEEN LONGERON 23 LEFT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: SKIN — CORRODED (BS 889-916)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH CORROSION BETWEEN Y889 AND Y916, LONGERON 28 LEFT AND 29 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 53-04. AREA WITHIN LIMITS IAW SRM 53-04 FIG 38. (M)

Part: SUPPORT — CORRODED (BS 889)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y889 LONGERON 27 LEFT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 51-01, FIG 1. (M)

Part: LONGERON — CORRODED (BS 945)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT ATTACH FITTINGS ON LONGERONS 25 RIGHT AND 26 RIGHT WITH CORROSION IN Y945. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 965)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y965 WITH CORROSION BETWEEN LONGERON 19 LEFT AND 23 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 935)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y935 WITH CORROSION BETWEEN LONGERON 25 LEFT AND 30 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: LONGERON — CORRODED (BS 869)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 29 RIGHT AND FRAME Y869 WITH CORROSION. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 889)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y889 WITH CORROSION BETWEEN LONGERON 29 RIGHT AND 27 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: CHANNEL — CORRODED (BS 756-775)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL WITH CORROSION SPOTS BETWEEN Y756 AND Y775 ON LONGERON 26 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: SKIN — CORRODED (BS 945-965)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN AND CHANNELS WITH CORROSION BETWEEN Y945 AND Y965 LONGERON 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1 AND 53-04 FIG 38. (m)

Part: LONGERON — CORRODED (BS 775)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FILLING SUPPORT FLOOR PANEL WITH CORROSION IN Y775 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: SUPPORT — CORRODED (BS 503)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CHANNEL WITH CORROSION BETWEEN Y503 AND Y522, LONGERON 21 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: LONGERON — CORRODED (BS 965-980)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 20, 21, 22 WITH CORROSION BETWEEN Y965 AND Y980 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: BEAM — CORRODED (CARGO COMPT)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT HORIZONTAL BEAM WITH CORROSION BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: LONGERON — CORRODED (BS 945-980)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 24 RIGHT WITH CORROSION BETWEEN Y945 AND Y980. REMOVED CORROSION AND TREATED METAL IAW 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: SUPPORT — CORRODED (BS 756-889)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL FLOOR SUPPORT PANELS WITH CORROSION BETWEEN Y 756 AND Y 889, LONGERON 27 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: LONGERON — CORRODED (BS 889-965)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 24 LEFT WITH CORROSION IN SEVERAL PLACES BETWEEN Y889 AND Y965. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: LONGERON — CORRODED (BS 446-465)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y446 AND Y465. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 446)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y446 WITH CORROSION BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW 53-01, FIG 1. (M)

Part: LONGERON — CORRODED (BS 503-522)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 25 RIGHT WITH CORROSION BETWEEN Y503 AND Y522. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 484)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y484 WITH CORROSION BETWEEN LONGERON 29 LEFT AND 29 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 503)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y503 WITH CORROSION BETWEEN LONGERON 28 RIGHT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 465)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y465 WITH CORROSION BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: LONGERON — CORRODED (BS 484-510)

DURIGN C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y484 AND Y510. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FITTING — CRACKED (BS 996)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT END FITTING, LONGERON 29 RIGHT WITH CRACK AND CORROSION IN Y996. REPLACED END FITTING IN LONGERON 20 RIGHT IAW SRM 51-01 PARA C AND 51-30-2, PART FABRICATED IAW SRM 51-10-2. (M)

Part: ANGLE — CRACKED (BS 832)

DTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y832 BETWEEN LONGERON 29 RT AND LONGERON 26 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M)

Part: ANGLE — CRACKED (BS 815)

DTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y 815 BETWEEN LONGERON 27 RT AND LONGERON 24 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M)

Part: ANGLE — CRACKED (BS 816)

DTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y816 BETWEEN LONGERON 28 RT AND LONGERON 24 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M)