N934ML

Part: CONNECTOR — DISCONNECTED (L1 DOOR)

ACY - FOUND L1 EMERGENCY EXIT IDENTIFIER INOPERATIVE. FOUND CANNON PLUG DISCONNECTED. RECONNECTED CANNON PLUG OPS CHECK GOOD IAW MM DC9 33-50-00. (M)

Part: WIRE — EXPOSED (CABIN)

DISCREPANCY: EMERG. FLOOR TRACK LIGHTING AT ROWS 14,17,18,23&15 HAVE EXPOSED WIRING. CORRECTIVE ACTION: READJUSTED AND SECURED EMERGENCY TRACK LIGHTING. OPS CHECKED GOOD IAW DC-9 M/M 33-50-0

Part: LIGHT — INOPERATIVE (CABIN)

FLL - FOUND EMERGENCY PATH LIGHT OUT AT EMERGENCY EXIT, RED LIGHT. REPLACED LAMP, OPS CHECKED OK. REF MM 33-51-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LGB- FLT 903 - AISLE PATH LIGHT OUT OF BOX IN FORWARD ENTRANCE. SECURED EMERGENCY FLOOR TRACK IT. COVER IAW DC-9 MM 33-50. OPS CHECK GOOD. (M)

Part: LIGHT — MISINSTALLED (CABIN)

DTW - FOUND EMERGENCY FLOOR TRACK LIGHTING STRIP AT 1 EF IS HELD DOWN BY CARGO PIT TAPE. RESECURED TRACK IAW 33-50-00, NO DEFECTS NOTED. (M)

Part: LIGHT — MISSING (CABIN)

FLL - AISLE FLOOR TRACK LIGHTING MISSING ONE RED LENS AT ROW 14 DEF. ASSIGNED DMI 91308-2 PER MEL 33-24 CAT C, DUE 4/11/00. (M)

Part: LENS — MISSING (CABIN)

DTW - EMERGENCY FLOOR TRACK LIGHTING AT ROW 19 MISSING LENS COVER AND LAMP. RELAMPED AND INSTALLED LENS COVER. OPS CHECK NORMAL IAW MM 33-51-1. (M)

Part: LENS — MISSING (CABIN)

TPA - EMERGENCY FLOOR PATH LIGHTING FOUND TO HAVE ONE RED LENS COVER AND BULB MISSING AFT OF AIRCRAFT. REPLACED MISSING BULB AND RES LENS COVER TO EMERGENCY EGRESS LIGHTING. OPERATIONAL CHECK PERFORMED FUNCTIONS. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

ISP - FLT 432 - EMERGENCY AISLE LIGHTING CAME ON IN FLIGHT AND WOULD NOT GO OUT. OPS CHECK SEVERAL TIMES ON GROUND NO DISCREPANCIES NOTED. (M)

Part: LIGHT — LOOSE (CABIN)

DTW - FORWARD EMERGENCY TRACK LIGHTING STRIP TEMPORARILY SECURED WITH SPEED TAPE. REPLACED EMERGENCY LIGHTING STRIP AND INSTALLED THRESHOLD PLATE IAW DC-9 SRM 51-30-2. (M)

Part: PLACARD — MISSING (CABIN)

DTW - FLT 91 - SOME OF THE SEATS THE PLACARDS 'LIFE VEST UNDER SEAT' ARE MISSING. REPLACED MISSING PLACARDS IAW DC9 MM 11-41-00. (M)

Part: WIRE — DAMAGED (CABIN)

MCO - FLT 92 - AFT ENTRY EMERGENCY 'EXIT' SIGN ON LEFT SIDE WALL INOPERATIVE. REPAIRED GROUND WIRE AT AFT ENTRY OVERHEAD. PANEL AND OPS CHECKED GOOD PER MM CHECK 33-50-00. (M)

Part: BATTERY — DISCHARGED (CABIN)

DTW - FLT 880 - AFT EMERGENCY EXIT (OVER WING) SIGNS (UPPER) WILL NOT LIGHT LEFT AND RIGHT. REPLACED BATTERIES IN EMERGENCY POWER PACK AT BS-25. OPS CHECK GOOD. REF: MD 80 MM 33-53-00. (X)

Part: SPLICE — FAILED (ROW 12)

ACY - FLT 880 - AISLE PATH LIGHTING FORWARD OF ROW 12 IS INOPERABLE. REPAIRED SPLICE, OPS CHECK GOOD. IAW MM 33-21-0. (X)

Part: BULB — FAILED (CABIN)

DTW - LEFT UPPER EMERGENCY LIGHT IS OUT. RELAMPED, OPERATIONS CHECKS GOOD AT THIS TIME. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DTW - ROW TWO EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPERATION CHECKS GOOD IAW DC-9 MM 33-50-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - CENTER OVERHEAD LIGHT EMERGENCY LIGHT BROKEN. CENTER OVERHEAD PANEL ASSEMBLY REMOVED. REPLACED BULB AND SOCKET TO CENTER OVERHEAD LIGHT (EMERGENCY ASSEMBLY. REINSTALLED PANEL ASSEMBLY. SYSTEM AROUND CHECKED GOOD ALL IAW DC-9 MM SECTION 33-00-0. (M)

Part: BATTERY PACK — DISCHARGED (LT NACELLE)

MYR - FLT 619 - LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 320. REMOVED AND REPLACED LEFT EMERGENCY NACELLE BATTERY PACK IAW MM CHAPTER 33-53-0. OPERATION CHECKS GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - AFT OVERHEAD EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED BULB AND SOCKET TO AFT OVERHEAD EMERGENCY LIGHT ASSEMBLY. SYSTEM CHECKED GOOD ALL IAW DC9 MM SECTION 33-00-00. (M)

Part: LIGHT — INOPERABLE (CABIN)

AFT CABIN DOOR EMERGENCY LIGHT (HAND HELD) INOPERATIVE. REMOVED AND REPLACED AFT CABIN DOOR EMERGENCY LIGHT ASSY IAW DC-9 MM 33-50-00. (X)

Part: SPRING — BROKEN (GALLEY DOOR)

MHV - FORWARD GALLEY DOOR ROLLER ASSY FOR THE DOOR BAYONET SPRING IS BROKEN ALLOWING THE ROLLER ASSY TO FLOAT WHEN THE DOOR IS BEING CLOSED. PERMITS BAYONET TO JAM BEHIND THE ROLLER ASSY. REMOVED AND REINSTALLED BROKEN SPRING WITH NEW ONE AW DC9 MM 52-41-0, PAGE 506. (X)

Part: FRAME — CRACKED (BS 560)

MHV - PASSENGER CABIN INTERNAL LEFT SIDE AT STA 560 AFT SIDE OF FRAME CRACKED APROXIMATELY 2 INCHES ABOVE FLOOR LINE. REMOVED FITTING FOR INSPECTION. REPAIRED DAMAGED AREA IAW DC9 SRM 51-01 AND SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-6. REINSTALLED FITTING IAW DC9 SRM 53-01 AND SRM 51-30-2. (X)

Part: BULB — FAILED (VENTRAL STAIRS)

DTW - AFT VENTRAL STAIRS SIDEWALL LIGHTS HAVE INOPERATIVE EMERGENCY LIGHT PORTION. RELAMPED CHECK GOOD AIW 33-50-00. (M)

Part: BATERY CHARGER — INOPERATIVE (CABIN)

DTW - CABIN, A NUMBER OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER STAND, CHECK GOOD IAW MM 33-50-00. (M)

Part: LIGHT — INOPERATIVE (ACCESSORY COMPT)

AFT ACCESSORIES COMPARTMENT CAT WALK MISSING EMERGENCY LIGHT LENSE AND BULB. REPLACED EMERGENCY LIGHT LENSE AND BULB IAW DC-9 MM 33-51-00. (M)

Part: PANEL — MISALIGNED (VERTICAL STAB)

MHV - REPLACEMENT VERTICAL UPPER CENTER PANEL PN 9911940-403 ATTACH HOLES DO NOT ALIGN WITH AIRCRAFT STRUCTURE. FABED IN REF TO DC9 SRM 51-10 MANUFACTURED FOLLOWING ITEMS. 2 EACH CHANNELS 1 EA RT. 1 EACH LT. 2 INCH Z-CLIPS, 1 EACH RT, 1 EACH LT. 2 BULKHEAD REPAIR ANGLES, 1 EACH RT. 1 EACH LT. HEAT TREATED AND AGED AS REQUIRED. SUPPLIED TO AIRCRAFT FOR FIT AND INSTALL ON WO A092-B10-N062. (X)

Part: PANEL — CRACKED (VERTICAL STAB)

MHV - VERTICAL STABILIZER CENTER PANEL UPPER, PN 9911940-403, HAS CRACK RT AFT SIDE APPROXIMATELY 8 INCHES LONG. CENTER PANEL REPAIR AND INSTALLATION TO BE ACCOMPLISHED ON A092-A03-N065. (X)

Part: STRUCTURE — DAMAGED (HORIZ STAB)

MHV - REMOVAL OF HORIZONTAL STABILIZER IS REQUIRED TO REPLACE WITH SERVICEABLE UNIT. REMOVED AND REPLACED HORIZONTAL STAB ASSY PER DC9 MM 55-10-0 PAGE 202. HORIZ STABILIZER ADJUSTMENT AND TEST C/W PER DC9 MM 55-10-0 PAGE 501 HORIZ STAB ACCESS PANELS WILL BE INSTALLED ON CARD A092A01M013. (M)

Part: PANEL — MISALIGNED (VERT STAB)

MHV - VERTICAL CENTER PANEL UPPER P/N 9911940-403 WHICH WAS REPLACED ON W/C NO062 HAS ATTACHING HOLES MISALIGNING WITH MATING HOLES ON VERT STRUT. PER ENG DWG NR 9909001 INSTALLATION COMPLETE PARTS FAB ON W/C A092-B10-N067 BRACKETS, CHANNELS, STRAPS ALL INSTALLED COMPLETE PER DC9 SRM 51-30-0 BANNONS FAIRING INSTALLED COMPLETE PER DC9 MM 55-10-0 AND PANEL 3521 ADN 3622. (M)

Part: FLOOR — WORN (BS 669-775)

MHV - LEFT CABIN FLOOR PANEL STATION 669 TO 775 SKIN AROUND NUMEROUS SCREW HOLES TO THIN. RESKINNED FLOOR PANEL IAW SRM DC9 53-20 AND 53-05, FABRICATED SKIN PANEL ALODINED AND PRIMED. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

MHV - PASSENGER CABIN STATION 484 LONGERON R6 INTERCOSTAL CRACKED. FABRICATED REPLACEMENT ITEM REF DC9 SRM 51-10 HEAT TREAT NOT REQUIRED ISSUED TO AIRCRAFT FOR FIT AND INSTALL ON W/O A092B03W106. (M)

Part: SUPPORT — CRACKED (BS 579-680)

MHV - CABIN CENTER LT FLOOR PANEL STA 579 TO STA 680 (BOTTOM OF FLOOR PANEL SUPPORT 2 AND 4 HAS CRACKS AND PUNCTURE HOLES). REMOVED SUPPORTS 2 AND 4 IAW SRM DC9 53-05 AND REPLACED SUPPORTS 2 AND 4 IAW SRM DC9 53-05. (X)

Part: STRINGER — MISDRILLED (BS 550-570)

MHV - PASSENGER CABIN INTERNAL STATION 550 TO 570 STRINGER L-17 THERE ARE APPROX 25 HOLES WITH SHORT C/C SPACING S/B .600 IAW SRM 53-02 FIG 18 SH 6 ARE .48-.58 REF NR A092-S03-W084. REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STATION 531 TO STATION 588 PRODUCTION SPLICE PER ENGINEERING DWG 53-99197-1 (CABIN PRESSURIZATION WILL BE ACCOMPLISHED ON WORK CARD NR A092A09Z025). (M)

Part: FLOORBEAM — MISMANUFACTURED (BS 996)

MHV - BS 996 FLOORBEAM UPPER CAP ANGLE FROM LBL 12 TO EOP AT LBL 52 REQUIRES NEW SECTION TO ACCOMMODATE LT AFT LAV FLOOR STRUCTURE MOD. C/W ENGINEERING DWG NR 53-99197-2. ALODINED AND PRIMED. (X)

Part: INTERCOSTAL — CRACKED (BS 484)

MHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO FACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 SRM 51-30-5 AND 51-10-4 PAGE 1 AND 4A FIG 3A. (M)

Part: SHEAR TIE — CRACKED (BS 940)

REMOVED B/S REPAIR RT FUSE CRACK IN SHEAR TIE APPRON STATION 940 BETWEEN STRINGER 15/16. FABRICATED ANGLE DOUBLER PER DC9 IAW SRM 51-10-2 PAGE 1 FIG 2 PER SAMPLE SUPPLIED. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

MHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO FACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 SRM 51-30-5 AND 51-10-4 PAGE 1 AND 4A FIG 3A. (M)

Part: FLOOR — CRACKED (BS 598)

MHV - CABIN CENTER RIGHT FLOOR PANEL STA 598 TO STA 639 HAS (5 EACH) CRACKS (3 EACH AT FASTENER HOLES AND TWO BELOW FASTENER HOLES). REPAIRED CRACKS INSTALLED DOUBLERS IAW SRM DC9 53-05 FAB DOUBLERS IAW SRM DC9 53-05 ALODINED AND PRIMED IAW SRM DC9 51-10-3. (X)

Part: WEB — CRACKED (BS 617)

MHV - CABIN STA 617 RBL 48, CRACK IN WEB. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. ALODINED AND PRIMED AND INSTALLED DOUBLER IAW SRM 53-01 FIG 2 (SHEET 3). (X)

Part: LONGERON — CRACKED (BS 560)

MHV - PASSENGER CABIN INTERNAL STA 560 LONGERON L-17 HAS A CRACK. HOLES WERE MIS-DRILLED. REPAIR WILL BE ACCOMPLISHED ON W/C NR A092-S39-W132. W132 - REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STA 531 TO STA 588, PRODUCTION SPLICE PER ENGINEERING DWG 53-99197-1 (CABIN PRESSURIZATION WILL BE ACCOMPLISHED ON WORK CARD NR 1092A09Z025). (X)

Part: STRINGER — CRACKED (BS 207)

MHV - BS 207 LT, STR 13 WEB IS CRACKED. RECEIVED VERIFICATION OF REPAIR MAT'L ON P.O. NR 80319. TRIMMED CRACKED MEMBER IAW DC9 SRM 53-01. ALODINED AND PRIMED IAW DC9 SRM 51-10-6. INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 53-01 AND SRM 51-30-2. (X)

Part: STIFFENER — CRACKED (RUDDER)

MHV - RUDDER RIB STIFFENER IS CRACKED, PN 5910256. FABBED NEW STIFFENER AND HEAT TREATED PER AMS-H 6080 AND DC9 SRM 51-10-2 PURCHASE AYA. PART REPAIR PART NOT REQUIRED. (X)

Part: SKIN — CRACKED (RUDDER)

MHV - THERE ARE 2 CRACKS ON THE RUDDER RIGHT SIDE AT RIB NR 6 AND RIB NR 8. REMOVED AND REPLACED RUDDER AND SKIN AND 1 STIFFENER IAW DC9 SRM 55-03 AND S/B 55-23R6 CNI AND AD87-08-03 W/B TO BE ACCOMPLISHED ON WO A092A03 N061. PAINT TO BE ACCOMPLISHED ON W/O A092P07F032. (M)

Part: SEALANT — DAMAGED (HORIZ STAB)

MHV - LEFT HORIZONTAL STABILIZER LIP EXTERIOR SURFACE THE SEALANT IS DAMAGE. NOT REQUIRED HORIZONTAL STAB REMOVED AND REPLACED ON W/C A092A03M058. (M)

Part: PANEL — WORN (HORIZ STABILIZER)

MHV - HORIZONTAL STABILIZER CENTER SECTION PANEL NR 3804A AFT AND LOWER SECTION WORN TO KNIFE EDGE. FABRICATED REPAIR DOUBLERS REF DC9 SRM 5503. HEATED TREATED AND AGE HARDENED PER AMS H 6088. ASSEMBLED AND ISSUED FOR INSTALLATION ON WO A092107022. (X)

Part: SKIN — CRACKED (HORIZ STAB)

MHV - HORIZONTAL STABILIZER CENTER SECTION UPPER RIGHT PANEL NR 3806A CRACKED AT AFT UPPER AREA ALSO WORN TO KNIFE EDGE. FABRICATED DOUBLER AND FILLER TO COVER DAMAGED PANEL, INSTALLED PER DC9 IAW SRM 55-03-0 PAGE 28 VIEW F ALODINE AND PRIMED PER DC9 IAW SRM 51-10-3 PAGE 16, 18 PARAGRAPH 23-30. (M)

Part: FLOOR — CRACKED (BS 669)

MHV - CABIN LT SIDE FLOOR PANEL STA 669 TO STA 775 CRACKED AT FASTENER HOLE WITH LIGHT SURFACE CORROSION AROUND FASTENER HOLES. SKIN REPLACEMENT NEEDED. COMPLETION OF WORK ON PANEL TO BE COMPELTED ON W122. (X)

Part: WIRE — BROKEN (ROW 20)

DTW - EMERGENCY FLOORTRACK LIGHTING FROM 20 THE ROW TO AFT CABIN DOOR INOPERATIVE, SIX LIGHTS. REPAIRED BROKEN WIRE. OPERATION CHECK GOOD IAW DC-9 MM 33-53-00. (M)

Part: BULB — FAILED (ROW 2)

DTW - OVERHEAD EMERGENCY LIGHT SYSTEM LEFT AND RIGHT LIGHTS INOPERATIVE AT ROW 2, LEFT AT ROW 4, AND RIGHT AT ROW 6. REMOVED AND REPLACED LAMPS, OPERATIONAL CHECK NORMAL IAW DC-9 MM CHAPTER 33-53-0. (M)

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT SYSTEM IN VENTRAL STAIRWAY UPPER LEFT INOPERATIVE. REPLACED BULBS, STILL INOPERATIVE. REPLACED BULBS IAW DC-9 MM 33-50-1. CHECKS GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FLT 417 - ON PREFLIGHT, FOUND FORWARD EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD NR 2 AND NR 4 BATTERIES IN BATTERY PACK ON EMERGENCY OVERHEAD LIGHTS. OPERATIONAL CHECK ON EMERGENCY LIGHTS GOOD DC-9 MAINTENANCE MANUAL 33-50-0. (M)

Part: SLIDE — SEPARATED (PASSENGER DOOR)

TPA - FLT 341 - PASSENGER ENTRANCE DOOR SLIDE PACK FELL OFF. RE-INSTALLED PASSENGER DOOR ENTRANCE SLIDE PACK IAW DC9 MM 25. (X)

Part: SLIDE — LOOSE (RT EMER EXIT DR)

THE RIGHT EXIT DOOR ESCAPE SLIDE FELL OUT OF THE CASING. INSTALLED COVERS ON RIGHT EMERGENCY ESCAPE SLIDE IAW DC-9 MM 25-61-0. (M)

Part: WIRE — BROKEN (CABIN)

DTW - EMERGENCY LIGHTS COME ON WITH BATTERY SWITCH IN OFF POSITION. FOUND NR 2 WIRE ON EMERGENCY LIGHT BATTERY PACK B5-5 BROKEN. REPAIRED WIRE, EMERGENCY LIGHT SYSTEM. OPS CHECK NORMAL ON GRUOND 33-53-0. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - EMERGENCY LIGHTS IN AFT CABIN STAY ON AT ALL TIMES. FOUND EMERGENCY LIGHTS BATTERY PACK B35-39, STATION 1000 FAULTY. REPLACED BATTERY PACK B5-39 AND FUNCTIONALLY TESTED SYSTEM IAW DC-9 MM 33-53-0. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - EMERGENCY LIGHTS IN CENTER CABIN INTERMITTENT. FOUND EMERGENCY LIGHT BATTERY PACK B5-25, STATION 639R, FAULTY. REPLACED B5-25 BATTERY PACK IAW DC9 MM 33-53-0. SYSTEM OPS CHECK NORMAL IAW DC-9 MM 33-53-0. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DTW - CEILING EMERGENCY LIGHTS ON LEFT SIDE BETWEEN ROWS 15-21 ARE OUT. REMOVED AND REPLACED BATTERY POWER SUPPLY WITH SERVICEABLE BATTERY POWER SUPPLY IAW DC-9 MM CH 33-58-0. OPS CHECK GOOD. (M)

Part: SLIDE — FELL OFF (GALLEY DOOR)

DTW - FLT 636 - GALLEY SERVICE DOOR SLIDE KEEPS FALLING OFF. RE-INSTALLED GALLEY SERVICE DOOR SLIDE IAW DC-9 MM 25-62-0. OPS CHECK GOOD. RII INSPECTION PERFORMED. (X)

Part: SLIDE — LOOSE (GALLEY DOOR)

DTW - FLT 174 - GALLEY DOOR SLIDE FALLING OUT OF PACK. RE-SECURED GALLEY DOOR SLIDE IAW DC-9 MM 25-61-00. RII INSPECTION ACCOMPLISHED. (M)

Part: GENERATOR — MALFUNCTIONED (LEFT)

DTW - FLT 703 - AFTER LEVELING AT CRUISE ALTITUDE, LEFT GENERATOR TRIPPED OFF LINE. SEVERAL RESET ATTEMPTS WERE UNSUCCESSFUL. USED APU TO CARRY LEFT BUSS. AFTER APPROXIMATELY 15 MINUTES, APU GENERATOR TRIPPED OFF LINE, WOULD'NT RESET. HOWEVER, LEFT GENERATOR DID RESET AND STAYED ON LINE. SEVERAL MINUTES LATER AN AC CROSS-TIE LOCKOUT OCCURRED, LTR VOLTS AND FREQS NORMAL. PERFORMED OPERATIONAL CHECKOUT OF AC GENERATION SYSTEM IAW DC 9 MM 24-20-0. SYSTEM CHECKED NORMAL. NO MALFUNCTIONS NOTED. (M)

Part: RELAY — FAILED (RIGHT)

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 RIGHT AUX 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 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 MX CONTROL. (M)

Part: CONNECTOR — LOOSE (CABIN)

DTW - FLT 626 - THREE FLOOR PATH EMERGENCY LIGHTS MISSING. RECONNECTED EMERGENCY PATH LIGHTS WITH BUTT SPLICE CONNECTOR. OPS CHECK GOOD, REF DC-9 MM 33-53-00. (M)

Part: BULB — MISSING (CABIN)

DTW - EMERGENCY FLOOR LIGHTING MISSING LIGHT BULB COVER, REFERENCE CABIN LOG CONTROL NR 8493, ITEM NR 3. REPLACED MISSING EMERGENCY FLOOR LIGHT COVER. OPERATIONAL CHECK OF FLOOR TRACK LIGHTING GOOD ON GROUND. (M)

Part: A/C SYSTEM — MALFUNCTIONED (LT ENGINE)

MCO - FLT 503 - CLIMBING THROUGH 700 FEET, LOSS OF L A/C DISTRIBUTION SYSTEM. PER FCOM, ATTEMPTED 1 RESET, UNSUCCESSFUL, L ENGINE GEN WILL NOT STAY ON LINE. CONCURRENTLY WITH ABOVE, A/C X-TIE LOCKOUT. PER FCOM, POWERED L, A/C DIST SYSTEM WITH APU GEN, AND CONTINUED. RESET GEN AND A/C X-TIE LOCKOUT IAW MM 24-20. PERFORMED ENGINE RUN UP AT GATE. ALL CONDITIONS CHECK NORMAL AT THIS TIME. PLEASE ADVISE NEXT FLIGHT. (M)

Part: WEBBING — OUT OF POSITION (EMERG EXIT DOOR)

MYR - FLT 112 - AFTER TAKEOFF DURING CLIMB, FA REPORTED EMERGENCY EXIT MAKING 'A LOT OF NOISE'. CAPTAIN CENTERED CABIN AND STATED DOOR LOOKED NORMAL, BUT WAS MAKING NOISE. RETURNED TO MYR FOR MAINTENANCE INSPECTION. INSPECTED EMERGENCY DOOR EXIT AND FOUND WEBBING IN DOOR SEAL. RE-INSTALLED WEBBING. INSPECTED DOOR SEAL. RE-INSTALLED EMERGENCY EXIT DOOR. OPS CHECK GOOD. (X)

Part: PRESS SWITCH — DEFECTIVE (RT ENGINE)

MYR - FLT 1702 - RIGHT OIL PRESSURE ANNUNCIATOR CAME ON DURING TAKEOFF WHEN POWER WAS SET. DEFERRED IAW MEL 79-2 EMI NR 00534. NOTED IN MYR. FOUND OIL LOW PRESSURE CAUTION SWITCH DEFECTIVE. REMOVED AND REPLACED FITTINGS AND REPLACED PRESSURE SWITCH IAW MM CHAPTER 78-32-2. (X)

Part: WIRE — LOOSE (CABIN)

DTW - FLT 621 - EMERGENCY FLOOR LIGHTING, LOCATED AT SEAT ROW 10, WIRE DETACHED. REPAIRED BROKEN WIRE IAW MM CH 33-53-0. OPS CHECK GOOD. (M)

Part: SLIDE — FELL OFF (GALLEY DOOR)

DTW - FLT 566 - GALLEY SERVICE DOOR SLIDE PACK CAME OFF. REPLACED GALLEY DOOR SLIDE PACK IAW DC9 MM 25-61. OPS CHECK GOOD. (M)

Part: SLIDE COVER — NOT SECURED (GALLEY DOOR)

MYR - FLT 561 - EMERGENCY SLIDE PACK COVER NOT SECURED ON SERVICE (GALLEY) ENTRY DOOR. REINSTALLED LOCK IN SLIDE COVER. OPS CHECK GOOD. (M)

Part: SLIDE — FELL OFF (GALLEY DOOR)

ACY - FLT 805 - SLIDE PACK FELL OFF DOOR. SECURED SLIDE PACK ON GALLEY DOOR IAW MM 25-61. (X)

Part: WIRE — BROKEN (RT OIL PRESSURE)

MYR - ON DAILY INSPECTION, FOUND RIGHT OIL PRESSURE INDICATOR READING INCORRECTLY. INSPECTED AND FOUND WIRING AT OIL PRESSURE TRANSMITTER CANNON PLUG BROKEN, RE-PINNED CANNON PLUG WIRING, RE-ROUTED, AND SECURED. PERFORMED ENGINE RUN. OPS CHECK GOOD IAW MM 79-30. (X)

Part: WIRE — BROKEN (CABIN)

DTW - AFT SUPPLY ROOM EMERGENCY 'EXIT' LIGHT INOPERABLE (BROKEN WIRE). FOUND WIRE PULLED OUT OF WIRE SPLICE. REPAIRED WIRE. LIGHT OPS CHECK GOOD. (X)

Part: BULB — MISSING (CABIN)

DTW - ROW 20 FLOOR TRACK LIGHTING MISSING BULB AND LENS. INSTALLED BULB AND LENS ON ROW 20 FLOOR TRACK LIGHTING. OPS CHECK GOOD. (X)

Part: SLIDE PACK — FELL OFF (GALLEY DOOR)

ACY - FLT 210 - ON POST FLIGHT SLIDE PACK FELL OFF GALLEY DOOR. INSTALLED SLIDE PACK BACK ON GALLEY DOOR PER MM 25-62-0. (M)

Part: BATTERIES — DIRTY (CABIN)

DFW - CABIN EMERGENCY LIGHTS IN CEILING REMAINED ILLUMINATED AFTER A/C SHUTDOWN AT HANGAR. REMOVED EMERGENCY BATTERIES, CLEANED ELECTRICAL CONTACTS AND REINSTALLED BATTERIES. OPS CHECK GOOD PER DC-9 MM 33-50 PAGE 408. (M)

Part: COMPUTER — FAILED (AUTOPITCH)

ACY - REFER TO DMI NR 00153 AUTOPILOT PITCH (MRR 97-2-11-002/GTIA9700161). REMOVED AND REPLACED AUTOPILOT PITCH AXIS COMPUTER IAW MM 22-13-1. TESTED GOOD IAW MM 22-13-1 SEC 3, PARAGRAPH A. CLEAR DMI 00153. (X)

Part: CONNECTOR — BAD WIRE (NR 2 ENGINE)

ACY - FLT 174 - DURING START NR 2 ENGINE HAD NO OIL PRESSURE. CIRCUIT BREAKER CHECKED, FCOM PROCEDURE COMPLETED. FOUND BAD WIRING AT OIL PRESS XMITTER. REPLACED CANNON PLUG AT XMITTER. OPS CHECK IAW 79-12-1. NO FAULTS FOUND. (M)

Part: AUTOPILOT — MALFUNCTIONED (E/E COMPARTMENT)

ACY - FLT 836 - AUTOPILOT PITCHES UP AND DOWN UNCONTROLLABLY. WILL NOT HOLD ALTITUDE. TRANSFERRED TO DMI LOG NR 00153 MEL 22-1 CAT 'C'. PLACARDS INSTALLED. (M)

Part: SWITCH — FAILED (RT ENGINE)

FLT 626 - RSW-DTW - EN ROUTE, DEPARTED WITH 13 QUARTS OF OIL IN RIGHT ENGINE. APPROXIMATELY 1 HOUR INTO FLIGHT OIL WAS 8 QUARTS AND DROPPING SLOWLY. DIVERTED TO ATL AND LANDED WITH 4 QUARTS OF OIL SHOWING ON GAUGE. REMOVED AND REPLACED OIL LOW PRESSURE WARNING SWITCH AND OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECK GOOD. LEAK CHECK GOOD. ALL WORK DONE IAW DOUG MM CHAP 79-32-00. (M)

Part: SWITCH — FAILED (RT ENGINE)

FLT 626 - RSW-DTW - EN ROUTE, DEPARTED WITH 13 QUARTS OF OIL IN RIGHT ENGINE. APPROXIMATELY 1 HOUR INTO FLIGHT OIL WAS 8 QUARTS AND DROPPING SLOWLY. DIVERTED TO ATL AND LANDED WITH 4 QUARTS OF OIL SHOWING ON GAUGE. REMOVED AND REPLACED OIL LOW PRESSURE WARNING SWITCH AND OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECK GOOD. LEAK CHECK GOOD. ALL WORK DONE IAW DOUG MM CHAP 79-32-00. (M)

Part: OIL PRESS SWITCH — MALFUNCTIONED (RT ENGINE)

FLT 625 - MCO - RT ENG SHUT DOWN DUE TO OIL QTY DEPLETION. OIL TEMP REMAINED NORMAL. OIL PRESS STARTED TO FLUCTUATE. OIL LEAKED DOWN TO 6 QTS SLOWLY THEN DEPLETED RAPIDLY. O/W LANDING 102,000 LBS. RT ENG OIL PRESS DIFF SWITCH IS BROKEN. INSPECT OIL SYS FOR FOREIGN MATTER. INSPECTED ENG FOR SIGNS OF LEAKAGE. REMOVED AND REPLACED NR 2 ENG OIL PUMP IAW MM CHAPTER 79-30. PERFORM ENG RUN AND LEAK CHECK, PERFORMANCE GOOD IAW MM CHAPTER 79-30. PERFORMED DETAILED INSPECTION IN REF TO O/W LANDING IAW DC-9 MM 5-51-0 PAGE 601-607. NO DEFECTS NOTED. REMOVED AND REPLACED OIL PRESS DIFF SWITCH AND PERFORMED ENG RUN. SYS CHECKS GOOD IAW MM 79-30. LEAK CHECK GOOD. (M)

Part: FLIGHT CONTROL — MALFUNCTION (RUDDER)

DTW - FLT 874 - ON CLIMB-OUT OF 8,000 FT, HEARD A LOUD BANG FROM REAR OF THE A/C. COULD NOT DETERMINE THE SOURCE, DECLARED AN EMERG AND RETURNED TO DTW. ALSO, EXPERIENCING UNCOMMANDED ROLL AND RUDDER FLUCTUATIONS WHICH INCREASED WITH SPEED ABOVE 10,000 FT. A/C WAS CLEAN, AIRFOIL AND ENG ANTI-ICE ON, THE YAW DAMPENER WAS ON, AUTO-PILOT WAS OFF. INSPECTED AIR CONDITIONING SYS AND DUCTING, INSPECTED AIL AND TAB IAW MM 27-10-0, INSPECT RUDDER AND TAB IAW MM 27-20-0, INSPECTED STAB TRIM IAW MM 27-40-1, INSPECTED ELEV AND TAB IAW MM 27-30-0, INSPECTED YAW DAMPENER IAW MM 22-11-0, INSPECTED SPOILER PANEL IAW MM 25-60-1, ALSO INSPECTED ENGS, MOUNTS, AND PYLONS. NO DEFECTS NOTED. COULD NOT LOCATE ANY DEFECTS ON A

Part: TRAP PANEL — CRACKED (LEFT)

DTW - ULTRASONIC AND EDDY CURRENT INDICATION CRACK EMANATING FROM NR 9 ATTACH HOLE IN UPPER AFT HORIZONTAL FLANGE OF LT TRAP PANEL. CRACK LENGTH APPROX 1 INCH. REPAIR ACCOMPLISHED IAW SB 53-182 AND DOUGLAS STRUCTURAL REPAIR MANUAL (SRM) 57-09 FIGURE 7A AND EA 5700-97-004. (M)

Part: STRUT — LEAKING (NLG)

DTW - FLT 509 - ON PUSH BACK, GROUND CREW NOTICED FLUID LEAKING FROM NOSE GEAR STRUT. REPACKED NOSE GEAR STRUT IAW DC-9 MM CHAPTER 32-21-2, NO LEAKS NOTED. (M)

Part: OXYGEN MASK — DEPLOYED (CABIN)

FLT 205 - FLL - PASSENGER OXYGEN MASKS DEPLOYED AT TOP OF CLIMB, 31,000 FEET, NO PRESSURIZATION PROBLEM PRESENT. BAROMETRIC SETTING WAS AT A VERY LOW SETTING WHICH CAUSED A HIGHER THAN NORMAL CABIN ALTITUDE. MAINTENANCE PERFORMED AN INSPECTION OF SYSTEM AND OPERATIONAL CHECK OF OXYGEN MASKS IAW DC9 MM, CHAPTER 35-20-3. ALL CHECK NORMAL AND MASKS STOWED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

DTW - FLT 1130 - RIGHT FORWARD EMERGNCY LIGHT TRACK BROKEN (LIGHTS WILL NOT STAY IN TRACK). MAINTENANCE REMOVED AND REPLACED PLASTIC RETAINER FOR FORWARD EMERGENCY PATH LIGHTING, OPS CHECK GOOD. (M)

Part: DOWNLOCK SW — FAILED (RT MLG)

DTW - FLT 626 - DURING LANDING GEAR EXTENSION EXPERIENCED A UNSAFE INDICATION ON RIGHT MAIN LANDING GEAR. RECYCLED LANDING GEAR, RIGHT MAIN GEAR REMAINED UNSAFE. LANDED DTW WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR DOWN LOCK POSITION SWITCH. OPERATIONAL CHECK GOOD IAW DC9 MM CHAPTER 32-60-1. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (RT ENGINE)

ACY - FLT 511 - DURING CLIMB CONFIGURATION RIGHT ENGINE OIL PRESSURE DECREASE TO 42 PSI, AND BEGAN FLUCTUATING BETWEEN 42 AND 40 PSI. OIL TEMPERATURE AND QUANTITY NORMAL. MAINTENANCE FOUND OIL PRESSURE TRANSMITTER CANNON PLUG LOOSE AND SOAKED WITH OIL. CLEANED AND SECURED CANNON PLUG. PERFORMED AN ENGINE RUN UP AND OIL PRESSURE NORMAL IAW DC9 MM CHAPTER 79-32-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RETRACT MECH — LACK OF LUBE (NLG DOOR)

BUF - FLT 856 - IN CLIMB CONFIGURATION WHEN LANDING GEAR RETRACTED, A LOUD FLUCTUATING SOUND WAS PRODUCED. SOUNDED LIKE NOSE LANDING GEAR DOORS. CORRECTIVE ACTION: MAINTENANCE INSPECTED NOSE LANDING GEAR DOORS, FOUND NOT TO BE SECURED. LUBRICATED NOSE GEAR DOOR LINKAGE, AND SECURED DOORS. OPERATIONAL CHECKED GOOD IAW DC 9 MM, CHAPTER 32. (X)

Part: BULBS — CORRODED (CABIN)

NUMEROUS CABIN EMERGENCY LIGHTS INOP. CLEANED SOCKETS AND REMOVED AND REPLACED CORRODED BULBS. (M)

Part: LIGHT — INOPERATIVE (CABIN)

L1 DOOR EMERGENCY LIGHT ASSEMBLY INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD PER 33-50-1. (M)

Part: WIRE — CHAFED (CABIN)

EMERGENCY EXIT LIGHT AT REAR EDGE OF GALLEY SERVICE DOOR CONTINUOUSLY FLICKER IN FLIGHT. FOUND WIRE CHAFED ON LIGHT ASSEMBLY. REPAIRED AS NECESSARY. (M)

Part: DUCT — FAILED (RT PACK)

CABIN DEPRESSURIZED, COULD NOT CONTROL IN MANUAL, CABIN OXYGEN MASKS DEPLOYED. FOD BLOWN DUCT BY RIGHT WATER SEPARATOR. REINSTALLED DUCT AND REPLACED PASSENGER OXYGEN MASKS. OPS CHECK OF OXYGEN MASKS CHECKED GOOD. (M)

Part: DOOR BEAM — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 6 REAR SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 6 REAR SECTION IAW SRM 52-05 FIG 31 SHEET 13 SECTION AC-AC PAGE 185. (M)

Part: FRAME — CORRODED (BS 1132.6)

DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y1132.6 AND LONGERON 16 LEFT CORRODED AND WORN. REPAIRED FUSELAGE FRAME IAW SRM 53-01 FIG 2 SHEET 4 PAGE 9. (M)

Part: FRAME — CRACKED (BS 1038)

DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y1038 AND LONGERON 13 LEFT CRACKED. REPAIRED FUSELAGE FRAME IAW SRM 53-01 FIG 2 SHEET 2. (M)

Part: SKIN — CORRODED (BS 667-756)

DURIGN C-CHECK, FOUND FUSELAGE SKIN SECTION FROM STATION Y667 TO STATION Y756, LONGERONS 28 LEFT TO 28 RIGHT CORRODED. REPLACED FUSELAGE SKIN SECTION IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2. (M)

Part: LONGERON — CORRODED (BS 563-604)

DURING C-CHECK, FOUND FUSELAGE 30 LONGERON SECTION FROM STATION Y563 TO STATION Y604 CORRODED. REPLACED FUSELAGE 30 LONGERON SECTION IAW COOPESA DWG HSE9-53-247, FAA FORM 8110-3 NR 95113 DATED NOV 30, 1995, AND FAA FORM 8110-3 NR 95112 DATED NOVE 30, 1995. (M)

Part: DOOR BEAM — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 2 AFT SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 2 AFT SECTION IAW SRM 52-05 FIG 31 SHEET 13 SECTION AA-AA PAGE 185. (M)

Part: FAIRING — DELAMINATED (LT ADF ANTENNA)

DURING C-CHECK, FOUND FORWARD ADF LEFT ANTENNA FAIRING DEFECTIVE DUE TO DELAMINATION. REPAIRED FORWARD ADF LEFT ANTENNA IAW COOPESA DWG HSE-9-53-270 DATED DEC 15, 1995 AND FAA FORM 8110-3 DATED DEC 15, 1995. (M)

Part: SEAT TRACK — CORRODED (BS 200-256)

DURING C-CHECK, FOUND PAX SEAT TRACKS FROM FS Y200 TO FS Y256 AT PLUS X23 AND -X47 CORRODED. REPAIRED PAX SEAT TRACKS IAW SRM 53-05 FIG 4 SHEET 1. (M)

Part: BULKHEAD TEE — CORRODED (BS 604)

DURING C-CHECK, FOUND FUSELAGE BULKHEAD T-CHORD SECTION AT Y604 BETWEEN LONGERONS 28 RIGHT AND 28 LEFT CORRODED. REPAIRED FUSELAGE T-CHORD SECTION IAW DOUGLAS FAX ACTION NR 284374 DATED DEC 6, 1995 AND MD DWG 5934768 VIEW 'C' ZONE 3 AND VIEW 'B' ZONES 8 AND 9. (M)

Part: DOOR PAN — CRACKED (LT MLG)

DURING C-CHECK, FOUND LEFT WHEEL WELL DOOR PAN INBOARD AFT SECTION CRACKED. REPAIRED LEFT WHEEL WELL DOOR PAN INBOARD AFT IAW COOPESA DWG HSE9-52-261 DATED DEC 7, 1995. (M)

Part: FRAME — CORRODED (BS 579)

DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y579 BETWEEN LONGERONS 27 RIGHT AND 27 LEFT CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A. (M)

Part: SKIN — CORRODED (BS 576-591)

DURIGN C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y576 AND STATION Y591, LONGERONS 28 RIGHT TO 28 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW COOPESA DWG HSE9-53-256 DATED DEC 4, 1995 AND FAA FORM DATED DEC 5, 1995. (M)

Part: SKIN — CORRODED (BS 988-996)

DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y988 AND STATION Y996, LONGERONS 29 RIGHT TO 29 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04, FIG 9 PAGE 23. (M)

Part: FRAME — CRACKED (BS 408)

DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y408 BETWEEN LONGERONS 25 LEFT AND 30 CRACKED AND CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEETS 1 TO 5. (M)

Part: JAMB — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR JAMB AT UPPER AFT CORNER CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR JAMB AT UPPER AFT CORNER IAW SRM 53-05 FIG 26A PAGE 62A. (M)

Part: SKIN — CORRODED (BS 667-756)

DURING C-CHECK, FOUND FUSELAGE SKIN SECTION FROM STATION Y667 TO STATION Y756, LONGERONS 28 RIGHT TO 28 LEFT CORRODED. REPLACED FUSELAGE SKIN SECTION IAW SRM 51-01 PARAGRAPH C AND SRM 51-30-2. (M)

Part: BULKHEAD WEB — CORRODED (BS 996)

DURING C-CHECK, FOUND FUSELAGE BULKHEAD WEB AT STATION Y996 FROM LONGERONS 23 RIGHT TO 23 LEFT AND BETWEEN -Z210 AND -Z240 CORRODED. REPLACED FUSELAGE BULKHEAD WEB IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 51-30-5. (M)

Part: FRAME — CORRODED (BS 917)

DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y917 BETWEEN LONGERONS 26 LEFT AND 29 RIGHT CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A. (M)

Part: SKIN — CORRODED (BS 589-607)

DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y589 AND STATION Y607, LONGERONS 17 RIGHT TO 19 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW COOPESA HSE9-53-263 DATED DEC 11, 1995 AND FAA FORM 8110-3 DATED DEC 11, 1995. (M)

Part: SKIN — CORRODED (BS 432-465)

DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y432 AND STATION Y465, LONGERONS 28 LEFT TO 29 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04 FIG 44 SHEET 1. (M)

Part: DOOR BEAM — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 6 FORWARD SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 6 FORWARD SECTION IAW SRM 52-05 FIG 31 SHEET 7 SECTION MM PAGE 193. (M)

Part: FAIRING — DELAMINATED (RT ADF ANTENNA)

DURING C-CHECK, FOUND FORWARD RIGHT ADF ANTENNA FAIRING DEFECTIVE DUE TO DELAMINATION. REPAIRED FORWARD RIGHT ADF ANTENNA IAW COOPESA DWG HSE9-53-262 DATED DEC 8, 1995 AND FAA FORM 8110-3 DATED DEC 11, 1995. (M)

Part: FLOOR — CORRODED (BS 237)

DURING C-CHECK, FOUND PAX CABIN AT Y237 TO X50 FLOOR OUTBOARD MEMBRANE CORRODED, FOUND DURING FORWARD TOILET FLOOR PANEL. REPLACED SHEET IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: FLOOR — CORRODED (BS 200-210)

DURING C-CHECK, FOUND PAX CABIN BETWEEN Y200 TO Y210 AND FROM XX23 TO XX49 PANEL CORRODED. LOCATED UNDER FLOOR PANEL. REPLACED SHEET UNDER FLOOR PANEL IAW SRM 51-0 PARA C. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: INTERCOSTAL — CORRODED (BS 237-256)

DURING C-CHECK, FOUND PAX CABIN INTERCOSTAL WITH CORROSION BETWEEN Y237 TO Y256 CENTER SECTION, FOUND DURING FLOOR PANEL REMOVAL. REPAIRED CHANNEL SUPPORT IAW EO-COO-9-53-165-95. (M)

Part: SUPPORT — CORRODED (CABIN)

DURING C-CHECK, FOUND PAX CABIN FORWARD LAVATORY FORWARD BULKHEAD BASE WITH CORROSION. REPLACED SUPPORTS OF FLOOR IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: DOOR FRAME — CORRODED (BS 427)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT Y427 AFT DOOR CUT OUT FRAME WITH CORROSION, AT ANCHOR NUTS ATTACHMENT POINTS BETWEEN LONGERON 25R AND 28R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01. (M)

Part: BULKHEAD ANGLE — CORRODED (BS 218)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT Y218 FORWARD BULKHEAD LOWER ANGLE WITH CORROSION BETWEEN LONGERON 25L AND 25R. REPAIRED ANGLE IAW SRM53-01, FIG 2 SHEET 4. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-0, FIG 1. (M)

Part: FRAME — CORRODED (BS 484)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y484 BETWEEN LONGERON 30 AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. AREA WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 503)

DURNIG C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y503 BETWEEN LONGERON 29L TO 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: FRAME — CORRODED (BS 332)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y332 BETWEEN LONGERON 29R AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: FRAME — CORRODED (BS 408)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION AND CRACKED ON LOWER FLANGE AT Y408 BETWEEN LONGERON 30 AND 25L. REPAIRED FRAME IAW SRM 53-03, FIG 2A, SHEET 1 OF 5 AT STATION Y408 FROM LONGERON 25L TO 30. (M)

Part: SKIN — CORRODED (BS 465-446)

DUIRNG C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL DOUBLER AND SKIN WITH CORROSION BETWEEN Y465 AND Y446 FROM LONGERON 29R TO 30. REPAIRED LOWER SKIN SECTION AND REPLACED DOUBLER BETWEEN Y432 AND Y465, LONGERONS 28L AND 29R IAW SRM 53-04, FIG 44 SHEET 1. (M)

Part: CHANNEL — CORRODED (BS 484-465)

DURING C-CHECK, FOUND FORWARD COMPARTMENT CHANNEL WITH CORROSION FROM Y484 TO Y465 BETWEEN LONGERON 30 AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)

Part: INTERCOSTAL — CORRODED (BS 332)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL WITH CORROSION BETWEEN Y351 AND Y332 AT LONGERON 29R. REPLACED INTERCOSTAL IAW SRM 51-01, PARA C. FABRICATED PART IAW SRM 51-10-2. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: SKIN — CORRODED (BS 332-351)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN AND DOUBLER WITH CORROSION BETWEEN Y332 AND Y351 FROM LONGERON 24R AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW 53-04, FIG 38. (M)

Part: SKIN — CORRODED (BS 541-560)

DURING C-CHECK, FOUND FWD CARGO COMPT INTERNAL SKIN WITH CORROSION BETWEEN Y541 AND Y560 AND FROM LONGERON 30 TO 29L. REMOVED CORROSION IN FWD CARGO COMPT INTERNAL SKIN BETWEEN Y541 AND Y560 AND FROM LONGERON 30 TO 29L, MATERIAL TREATED IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-04 FIG 38. (M)

Part: ANGLE — CORRODED (BS 439)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT ANGLE WITH CORROSION AT Y439 BETWEEN LONGERON 29L AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: LONGERON — CORRODED (BS 389-465)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 29L WITH CORROSION AND CRACKED BETWEEN Y389 AND Y465. REPLACED 29L LONGERON SECTION FROM Y389 TO Y465 IAW EO NR 000-9-53-172-95. (M)

Part: INTERCOSTAL — CORRODED (BS 579-598)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL WITH CORROSION AND CRACKED BETWEEN Y579 AND Y598 AND BETWEEN LONGERONS 28L AND 27L. REPLACED DAMAGED INTERCOSTAL IAW SRM 51-01 PARA C. TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW 51-30-2. FABRICATED INTERCOSTAL IAW SRM 51-10-2. (M)

Part: SUPPORT — CORRODED (BS 590)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT WITH CORROSION AT Y590 BETWEEN LONGERON AND 26R AND 26L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW 53-01 FIG 1. (M)

Part: SKIN — CORRODED (BS 503)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN WITH CORROSION BETWEEN LONGERON 29L AND 29R FROM Y484 TO Y503. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. AREA WITHIN LIMITS IAW SRM 53-04, FIG 38 TABLE A. (M)

Part: LONGERON — CORRODED (BS 351-332)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 29R WITH CORROSION BETWEEN Y351 AND Y332. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1, SHEET 3. (M)

Part: SUPPORT — CRACKED (BS 362.5)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CRACKED AT 7362.5 BETWEEN LONGERON 28R AND 27R. REPLACED FLOOR SUPPORT IAW RM 51-01 PARA C. FABRICATED PART IAW SRM 51-10-2. REPLACED HI-LOCKS IAW SRM 51-30-5. (M)

Part: FRAME — CORRODED (BS 389)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y389 BETWEEN 29L AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITH IN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: CHANNEL — CORRODED (BS 598.5)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR CHANNEL WITH CORROSION BETWEEN Y439 AND Y598.5 FROM LONGERON 28R AND 27R. REMOVED CORROSION AND TREATED METAL IN CHANNEL SECTION BETWEEN Y470 AND Y598.5 LONGERONS 27 AND 28R IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED DAMAGE SECTIONS BETWEEN Y433 AND Y470 IAW SRM 51-01 PARA C. INSTALLED RIVETS AND ANCHOR NUTS IAW SRM 51-30-2. (M)

Part: SKIN — CORRODED (BS 446-427)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN WITH CORROSION BETWEEN Y446 AND Y427 FROM LONGERON 28R AND 29L. REMOVED CORROSION AND TREATED MATERIAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: INTERCOSTAL — CORRODED (BS 579-598)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL WITH CORROSION BETWEEN Y579 AND Y598 AND BETWEEN LONGERON 28R AND 27R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-01 PARA C AND SRM 51-10-3. INSTALLED RIVETS IAW SRM 51-30-2. FABRICATED INTERCOSTAL IAW SRM 51-10-2. (M)

Part: SKIN — CORRODED (BS 362.5)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN WITH CORROSION AND SCRATCHES BETWEEN Y362.5 AND Y427 FROM LONGERON 29L TO 29R. REMOVED DOUBLER, CORROSION AND SCRATCHES AND TREATED METAL FROM Y362.5 AND Y427, BETWEEN LONGERONS 29L TO 29R IAW 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-04 FIG 38. REINSTALLED DOUBLERS AND RIVET IAW SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 541)

DURING C-CHECK, FOUND FCC FRAME WITH CORROSION ON LOWER FLANGE AT Y541 BETWEEN LONGERONS 29L AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 PG 20. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: JAMB — CRACKED (BS 439-362.5)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INNER SKIN OF DOOR JAMB DENTED, CRACKED AND CORRODED BETWEEN Y439 AND Y362.5 FROM LONGERON 29R TO 24R. REPLACED SKIN SECTION IN LOWER DOOR FRAME SECTION OF FWD CARGO COMPT BETWEEN Y439 TO Y362.5, LONGERON 29 AND 24R IAW SRM 51-01 PARA C. INSTALLED RIVETS IAW SRM 51-30-2. FABRICATED MATERIAL IAW SRM 51-10-2. (M)

Part: JAMB — CORRODED (BS 427-370)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LOWER DOOR CUT OUT, JAMB WITH CORROSION BETWEEN Y427 AND Y370. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: CHANNEL — CORRODED (BS 362.5-218)

DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR CHANNEL WITH CORROSION BETWEEN Y362.5 AND Y218 AND BETWEEN LONGERON 28R AND 27R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1, BETWEEN Y362.5 AND Y218. REPLACED DAMAGE FLOOR CHANNEL SECTIONS IAW SRM 51-01 PARA C BETWEEN Y363 AND Y304. INSTALLED RIVETS AND ANCHOR NUTS IAW SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 200)

DURING C-CHECK, FOUND E/E COMPARTMENT FRAME CORRODED AT STATION Y200 BETWEEN LONGERON 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 917)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME STATION Y917 WITH CORROSION BETWEEN LONGERONS 26 LEFT AND 29 RIGHT. REPAIRED DAMAGED FRAME SECTION AT Y917 BETWEEN LONGERONS 26 LEFT AND 29 RIGHT IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A, FABRICATED SPLICE IAW SRM 51-10-2. (M)

Part: FRAME — CORRODED (BS 937)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME STATION Y937 AFT FACE WITH CORROSION BETWEEN LONGERONS 26 LEFT AND 29 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 170)

DURING C-CHECK, FOUND E/E COMPARTMENT LONGERON 29 RIGHT WITH LIGHT CORROSION AT STATION Y170. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: FRAME — CORRODED (BS 897)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME STATION Y897 AFT FACE FRAME WITH CORROSION BETWEEN LONGERON 26 LEFT AND 30 FRAME. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: LONGERON — CORRODED (BS 980-996)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y980 AND Y996. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: FLOOR — CORRODED (BS 197)

DURING C-CHECK, FOUND E/E COMPARTMENT PAX CABIN FLOOR PANEL WITH CORROSION AT Y197 AND X20. REPLACED SHEET IN FLOOR PANEL IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-70-2. (M)

Part: ANGLE — CORRODED (BS 218)

DURING C-CHECK, FOUND E/E COMPARTMENT FLOOR SUPPORT ANGLE WITH CORROSION AT STATION Y218 BETWEEN LONGERON 29R AND 29L. REPLACED DAMAGED ANGLE IAW SRM 51-01 PARA C. FABRICATED ANGLE IAW SRM 51-10-2, TREATED METAL IAW SRM 51-10-20. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 180)

DURING C-CHECK, FOUND E/E COMPARTMENT STATION Y180 FRAME CORRODED BETWEEN LONGERON 29R AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: BASE — CORRODED (BS 218)

DURING C-CHECK, E/E COMPARTMENT ANTENNA MOUNTING BASE WITH CORROSION AT STATION Y218 BETWEEN LONGERON 30 AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: CHANNEL — CORRODED (BS 794)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR CHANNEL LEFT WITH CORROSION AND LOOSE RIVETS BETWEEN Y794 AND Y809. ACCOMPLISHED REPAIR AT AFT C/C FLOOR CHANNEL LEFT BETWEEN Y813 AND Y832, Y794 AND Y813 IAW SRM 53-02 FIG 2 SHEET 4. (M)

Part: LONGERON — CORRODED (BS 813-869)

DURING C-CHECK, FOUND AFT CARGO COMPT LONGERON 30 WITH CORROSION BETWEEN Y813 AND Y869. REMOVED CORROSION AND TREATED METAL SECTION IAW SRM 51-10-3 AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 851)

DURING C-CHECK, FOUND AFT CARGO COMPT FRAME WITH CORROSION IN BOTH FACE AT Y-851 BETWEEN LONGERON 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. SECTION WITHIN LIMITS IAW SRM 53-01 FIG 1 SHEET 3. REPLACED RIVETS IAW 51-30-2. (M)

Part: FRAME — CORRODED (BS 869)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME WITH CORROSION AT Y869 BETWEEN LONGERON 29 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 869-945)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y869 AND Y945. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: INTERCOSTAL — CORRODED (BS 889-897)

DURING C-CHECK, AFT CARGO COMPARTMENT INTERCOSTAL WITH CORROSION BETWEEN Y889 AND Y897 AND BETWEEN LONGERONS 30 AND 29 RT. REPLACED INTERCOSTAL BETWEEN Y889 AND Y897 AND LONGERON 30/29 RIGHT IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-30-2. FABRICATED UNIT IAW SRM 51-10-2. (M)

Part: LONGERON — CORRODED (BS 897)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 23 LEFT STRAP WITH CORROSION AT Y897. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: LONGERON — CORRODED (BS 869-889)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 29 RIGHT WITH CORROSION BETWEEN Y869 AND Y889. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 53-30-2. (M)

Part: SPLICE — CORRODED (BS 794-813)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 30 SPLICE WITH CORROSION BETWEEN Y794 AND Y813. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: FRAME — CORRODED (BS 869)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME WITH CORROSION AT Y869 BETWEEN LONGERONS 26 AND 25 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: SKIN — CORRODED (BS 794-813)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH CORROSION BETWEEN LONGERON 30 AND LONGERON 29 LEFT AND BETWEEN Y794 AND Y813. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1 SHEET 3. INSTALLED RIVETS IAW SRM 51-30-2. (M)

Part: FITTING — CORRODED (BS 996)

DURING C-CHECK, AFT CARGO COMPARTMENT LONGERON 230C END FITTING WITH CORROSION AT STATION Y996. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: CHANNEL — CORRODED (BS 996)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR CHANNEL RIGHT WITH CORROSION BETWEEN Y945 AND Y996. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: FRAME — CORRODED (BS 832)

DURING C-CHECK, FOUND AFT CARGO COMPT FRAME WITH CORROSION AT Y832 BETWEEN LONGERONS 28 LT AND 29 RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: FRAME — CORRODED (BS 775)

DURING C-CHECK, AFT CARGO COMPARTMENT FRAME WITH CORROSION IN LOWER FLANGE IN Y775 BETWEEN LONGERON 30 AND LONGERON RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: CHANNEL — CORRODED (BS 756-889.5)

DURING C-CHECK, FOUND AFT CARGO COMPT FLOOR CHANNEL RIGHT WITH CORROSION AND LOOSE RIVETS BETWEEN Y756 AND Y889.5. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1 AND REPLACED RIVETS IAW SRM 51-30-2. (M)

Part: SKIN — CORRODED (BS 756)

DURING C-CHECK, AFT CARGO COMPARTMENT SKIN WITH CORROSION BETWEEN LONGERON 29 RIGHT AND 30 AT Y756. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: FRAME — CORRODED (BS 794)

DURING C-CHECK, AFT CARGO COMPARTMENT FRAME WITH CORROSION IN LOWER FLANGE AND FORWARD FACE AT Y794 BETWEEN LONGERON 29 LEFT AND LONGERON 30. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)

Part: FRAME — CORRODED (BS 813)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME WITH CORROSION IN LOWER FLANGE AND FORWARD FACE AT Y813 BETWEEN LONGERON 29LT AND LONGERON 28RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M)