N928ML

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - LEFT FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED B5-32 BATTERY PACK IAW MM 24-30-0. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (M)

Part: SLIDE — DEPLOYED (L1 DOOR)

L-1 DOOR SLIDE PACK FELL TO GROUND AND DEPLOYED. REPLACED L-1 DOOR SLIDE PACK IAW DC-9 MM 25-61-00. (M)

Part: SLIDE — DETACHED (R1 DOOR)

DTW - SLIDE PACK ON R-1 DOOR FELL FROM THE DOOR ONTO THE CARPET GALLEY FLOOR DURING CLEANING PROCEDURE. RE-INSTALLED SLIDE PACK ON R-1 DOOR IAW MM 25-61-00. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES POWER PACK ASSEMBLY. OPERATION CHECKS GOOD. (X)

Part: BATTERY — DISCHARGED (CABIN)

ACY - FLT 286 - OVERHEAD EMERGENCY LIGHT IN COCKPIT INOPERATIVE. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. REMOVED AND REPLACED 2 EACH BATTERIES ON EMERGENCY LIGHT PACK, OPERATIONS CHECK GOOD. (M)

Part: WIRE — BROKEN (CABIN)

FRONT WHITE EMERGENCY FLOOR LIGHT OUT. REPLACED SOCKET AND LENS AND LAMP TO FRONT EPL LIGHT AND REPAIRED BROKEN WIRES. OPERATION CHECK NORMAL. (M)

Part: WIRE — BROKEN (CABIN)

MCO - AFT EMERGENCY FLOOR PATH LIGHTING, ONE EACH. RED LIGHT INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD PER MM 33-51-0. (X)

Part: LIGHT — INOPERATIVE (OVERWING EXIT)

DTW - EMERGENCY FLOOR TRACK LIGHTING HAS AN INOPERATIVE BULB (RED AT OVERWING EXIT). REINSTALLED LOOSE BULB IN RECEPTACLE. OPERATION CHECKS GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FLT 558 - DURING DAILY, FOUND AFT TAIL CONE EMERGENCY LIGHTS INOPERATIVE. FOUND BATTERY PACK AT R-27 IN AFT LAVATORY INOPERATIVE. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK IAW MM 33-53-0. OPERATIONAL CHECKS GOOD. (M)

Part: SLIDE — LOOSE (CABIN)

MYR - FLT 381 - SLIDE PACK CAME LOOSE FROM GALLEY DOOR. REINSTALLED SLIDE PACK COVER AND SLIDE ON GALLEY DOOR RIGHT SIDE OF AIRCRAFT. (M)

Part: BULB — MISSING (CABIN)

DTW - FLT 418 - LIGHT BULB MISSING FROM RED AISLE PATH LIGHT AT ROW 14. RELAMPED EMERGENCY TRACK LIGHT AT ROW 14. OPERATIONAL CHECK GOOD. REFERENCE DC-9 MM CHAPTER 33-50-00. (M)

Part: LIGHT — INOPERATIVE (CABIN)

EWR - FLT 264 - CABIN LOG ITEM NR 3, FLOOR PATH LIGHTING AT EXIT ROW IS MISSING A RED LIGHT. REPLACED LIGHT AND LENS COVER, OPERATIONAL CHECK GOOD. (M)

Part: BULB — FAILED (CABIN)

DTW - EMERGENCY FLOOR TRACK LIGHTING 2 BULBS INOPERATIVE. REPLACED 2 BULBS IN EMERGENCY FLOOR TRACK LIGHTING. OPERATIONAL CHECK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

GTIA - EMERGENCY EXIT LIGHT ABOVE VENTRAL DOOR WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK. EMERGENCY EXIT LIGHT ABOVE VENTRAL DOOR WILL NOT EXTINGUISH. OPERATIONAL CHECK GOOD. (X)

Part: LIGHT — FAILED (CABIN)

SECTION OF EMERGENCY FLOOR TRACK LIGHTING IS INOPERATIVE (TOWARDS REAR OF CABIN). REPAIRED FAULTY WIRE (PULLED FROM BUTT SPLICE) OPERATION GOOD. REFERENCE: MM 33-50-0. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND BROKEN WIRE AND BAD TERMINAL STRIP ON BATTERY POWER SUPPLY PACK AT 5-32. REMOVED AND REPLACED BATTERY POWER SUPPLY PACK PER DC-9 MM 33-53-0 AND REPAIRED BROKEN WIRE PER DC-9 MM 20-50-1, OPERATIONAL CHECK GOOD. (X)

Part: BULBS — FAILED (CABIN)

DTW - AFT COMPARTMENT FLOOR EMERGENCY LIGHTS BURNED OUT. REMOVED AND REPLACED EMERGENCY LIGHT LAMPS AS REQUIRED IAW DC9 MM CHAPTER 33-50-0. (X)

Part: WIRE — LOOSE (CABIN)

DTW - ONE LIGHT IN FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE AT 17D, LENS COVER IS MISSING. REATTACHED LOOSE WIRE AND REPLACED BULB AND LENS COVER AS REQUIRED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - ON DAILY CHECK, FOUND FWD PORTABLE E LIGHT AT AFT F/A STATION INOP. REMOVED AND REPLACED AFT F/A STATION FWD E LIGHT. INSTALLATION CHECKS GOOD IAW DC-9 MM 33-53-0. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 411 - FLL - REAR CABIN FWD EMERGENCY FLASHLIGHT SAFETY WIRE BROKEN AND APPEARS INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT. OPS CHECK GOOD IAW MM REF 2550. (M)

Part: LENS — MISSING (CABIN)

DTW - EMERGENCY AISLE PATH LIGHTING (1ST LIGHT) PROTRUDING FROM FLOOR. REPLACED LENS COVER IAW DC-9 MM 33-50. OPS CHECK GOOD. (M)

Part: CONNECTOR — DIRTY (RT ENGINE)

PIE - FLT 220 - RIGHT ENGINE FIRE DETECTOR LOOP 'A' LIGHT CAME ON FOR A FEW SECONDS AND THEN WENT OUT. SYSTEM TESTS OK. CLEANED OILY CONNECTORS ON LOOP 'A' FIRE DETECTOR. FIRE DETECTOR TEST NORMAL. (M)

Part: CLIPS — OUT OF ADJUST (GALLEY SLIDE)

GALLEY SLIDE FALLS OFF A SLIGHTEST MOVEMENT. ADJUSTED CLIPS. OPS CHECK NORMAL IAW MM CHAPTER 25-62-0. (X)

Part: CONNECTOR — LOOSE (NLG)

PIE - FLT 116 - WHEN NOSE GEAR WAS LOWERED, THERE WAS NO INDICATION OF EITHER SAFE OR UNSAFE WHEN THROTTLES WERE PULLED BACK. NO GEAR HORN NOTED. FOUND NOSE GEAR DOWNLOCK SWITCH CONNECTOR LOOSE AND DIRTY. CLEANED AND RE-INSTALLED CONNECTOR TO DOWNLOCK SWITCH ON NOSE GEAR. SYSTEM OPS CHECK OK PER DC-9 MM 32-60. (X)

Part: LATCH MECHANISM — OUT OF ADJUST (LT/RT MLG DOOR)

PIE - FLT 220 - LEFT MAIN GEAR UNSAFE LIGHT CAME ON DURING DESCENT FOLLOWED BY VIBRATION. PUT RIGHT HYDRAULIC PUMP ON HIGH. LIGHT WENT OUT AND VIBRATION STOPPED. REDUCED SPEED BELOW 300 KNOTS. AIRCRAFT INSPECTED FOR FERRY FLIGHT TO DTW. FOUND TO BE OK FOR MAINTENANCE FERRY TO DTW. ADJUSTED LT AND RT MAIN GEAR DOOR LATCH MECHANISMS IAW DC-9 MM 32-31-4. (X)

Part: STRIKER BOLT — OUT OF ADJUST (LT MLG DOOR)

ACY - FLT 357 - ON DEPARTURE WITH GEAR SELECTOR UP, LEFT GEAR UNSAFE ILLUMINATED. GEAR WAS RECYCLED DOWN, GEAR DOOR LIGHT REMAINED ON. ADJUSTED LEFT GEAR DOOR SWITCH STRIKER BOLT IAW 32-31-4. ALL LIGHTS OPS CHECK NORMAL. (X)

Part: STRIKER — LOOSE (LT MLG DOOR)

DTW - FLT 559 - AFTER TAKEOFF/GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ACCOMPLISHING QRH PROCEDURES AND RECYCLING GEAR CAUSED GEAR DOOR OPEN LIGHT TO REMAIN ILLUMINATED AFTER GEAR EXTENSION. QRH REFERENCED CONFIRMATION OF GEAR DOOR POSITION VISUALLY, GEAR DOOR VISUALLY CONFIRMED TO BE IN THE UP POSITION. NORMAL LANDING AND TAXI TO THE GATE IN DETROIT. FOUND LEFT GEAR DOOR SWITCH STRIKER LOOSE. ADJUSTED AND SECURED LEFT GEAR DOOR SWITCH STRIKER. LEFT GEAR DOOR OPS CHECK NORMAL. (M)

Part: WIRE — CHAFED (CABIN)

DTW - EMERGENCY FLOOR TRACK IN TAIL IS INOPERABLE. FOUND CHAFFED WIRE IN TAIL FLOOR TRACK LIGHTING ASSEMBLY. REPAIRED AS REQUIRED. SYSTEM OPS CHECK GOOD IAW DC9 MM CH 33-50. (M)

Part: UPLIMIT SWITCH — FAILED (LT MLG)

PIE - FLT 220 - DEPARTING EWR, UPON GEAR RETRACTION, 'LEFT GEAR UNSAFE' AND 'GEAR DOOR OPEN' LIGHTS REMAINTED ILLUMINATED. REFERRED TO ABNORMALS CHECK LIST 'RED LIGHT ON WITH GEAR HANDLE UP'. CYCLED L/G, LIGHTS EXTINGUISHED AND UPLOCK CHECKED GOOD. CONTINUED FLT. INSPECT MLG LEFT DOOR LATCH PER MM 32-31-4. ALL MEASUREMENTS FOR CATCH ASSY GOOD. FOUND TRACES OF DIRT IN UPLOCK SWITCH CANNON PLUG. CLEANED CANNON PLUG THOROUGHLY AND RE-INSTALLED. CLEANED CANNON PLUG FOR GEAR DOOR SW LIGHTS. OPS CK NORM PER 32-60-1. R/R'D LEFT MLG UPLIMIT SW IAW 32-60-1. UNIT OPS CHECK GOOD. (M)

Part: COVER — MISSING (CABIN)

PIE - TRANSFERRED FROM CABIN LOG EMERGENCY TRACK BULB COVER IS MISSING. RELAMPED EMERGENCY LIGHT AND REINSTALLED TRACK LENS. OPS CHECK GOOD. (M)

Part: WIRE — BROKEN (RT MLG)

ACY - FLT 220 - DEPARTING EWR THE GEAR HANDLE WAS RAISED. GREEN LIGHTS WENT OUT. LEFT MAIN UNSAFE LIGHT REMAINED ON. RECYCLED THE LANDING GEAR. ALL THREE GREEN LIGHTS ILLUMINATED. THE GEAR HANDLE WAS RAISED, THE MAIN RED BOTH UNSAFE LIGHTS REMAINED ON ALONG WITH THE GEAR DOOR OPEN LIGHT. ON APPROACH TO ACY WITH THE AIRSPEED BELOW 180 KTS THE RED UNSAFE LIGHTS WENT OUT ALONG WITH THE GEAR DOR OPEN LIGHT. LANDING GANG TAXI WERE NORMAL. (M)

Part: DOOR LATCH — OUT OF ADJUST (RT MLG)

RSW - FLT 214 - AFTER TAKEOFF LEFT GEAR UNSAFE LIGHT STAYED ON. WHILE PERFORMING ABNORMAL PROCEDURES FOR 'RED LIGHT ON GEAR HANDLE UP' GEAR DOOR. OPEN LIGHT STAYED ON UNTI AIRCRAFT WAS SLOWED BELOW 20 KTS. GEAR DOOR OPEN LIGHT COMES ON ABOUT 200 KTS AND GOES OUT BELOW 200 KTS. HYD PUMPS WERE ON HIGH AT ALL TIMES, RETURNED TO RSW. ADJUSTED RIGHT GEAR DOOR LATCH STOP AS PER DC-9 MM 32-31-4. OPS CHECK GOOD ON GROUND. (M)

Part: RETRACT MECH — MALFUNCTIONED (SPEED BRAKES)

ACY - FLT 177 - SPEED BRAKE, IN-FLIGHT, PRODUCES A ROLL TO THE RIGHT WHEN FULLY EXTENDED. WOULD NOT STOW WHEN RETRACTED. PHYSICALLY INSPECTED SPOILERS FOR SECURITY IN EXTENDED/RETRACTED POSITION. SYSTEM OPERATION CHECK NORMAL IAW 27-60-0. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - SPEED TAPE ON EMERGENCY TRACK LIGHTING TOWARDS FRONT. REMOVED SPEED TAPE AND REPLACED SECTION OF BAD TRACK AS REQUIRED IN MM CHAPTER 33-50. (X)

Part: SMOKE DETECTOR — MALFUNCTIONED (RT LAVATORY)

AFT LAV SMOKE ALARM ACTIVATED IN FLIGHT, NO SMOKE IN LAVATORY. ALARM WAS TEMPORARILY SILENCED WHEN TEST SWITCH ACTIVATED, BUT THEN ALARM WAS CONSTANT. DEFERED RT LAVATORY IAW MEL 26-7 DMI NR 00548 CAT 'C' DUE 5-29-97. TRASH CHECKED AND DOOR LOCKED. REMOVED AND REPLACED SMOKE DETECTOR IAW DC9 MM 26-26. OPS CHECK GOOD. THIS CLEARS DMI NR 00548. (M)

Part: SMOKE DETECTOR — JAMMED SWITCH (LAVATORY)

DTW - FLT 640 - AFT LAV SMOKE DETECTOR ACTIVATED SPURIOUSLY IN-FLIGHT. FOUND TEST SWITCH JAMMED IN CLOSE TO TEST MODE. UN-JAMMED SWITCH. SEVERAL OPS CHECKS COMPLETED. ALL CHECKS GOOD. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DW - FLT 1702 - CABIN EMERGENCY LIGHTS (OVERHEAD) OUT. SYSTEM OPS CHECK GOOD IAW DC-9 MM 33-50. NO DEFECTS AT THIS TIME.

Part: DIMMING BOX — FAILED (RT MLG)

DTW - FLT 621 - AFTER TAKEOFF, RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR LIGHT REMAINED ON. REMOVED AND REPLACED GEAR LIGHT DIMMING BOX. REPAIRED PINS 28 AND 34 ON P1-79 (DIMMING BOX CONNECTOR). REMOVED AND REPLACED RIGHT MAIN 51-84 GEAR SWITCH AS A PRECAUTIONARY MEASURE. ALSO, REPLACED RIGHT HAND GEAR DOOR LOCK CONNECTOR. PERFORMED EXTENSION/RETRACTION REPEATEDLY PER DC-9 MM CHAPTER 32-30-0. OPS CHECK NORMAL WITH NO FAULTS AND NO DISCREPANCIES NOTED. (X)

Part: CONNECTOR — DIRTY (NLG)

MYR - FLT 181 - ON APPROACH, NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE. VERIFIED DOWN THROUGH PERISCOPE AND FCOM PROCEDURES. INSPECTED NOSE LANDING GEAR, FOUND GEAR DOWN AND LOCKED. NO DEFECTS NOTED. CLEANED SWITCH AND CANNON PLUG. SYSTEM OPS CHECK GOOD. (M)

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR)

DTW - FLT 626 - AFT CARGO DOOR LIGHT CAME ON. FOLLOWED FCOM. PRESSURIZATION WAS OK. CLEANED CARGO DOOR (FWD) SWITCH. PERFORMED TEST IAW MM CHAPTER 52-70-0. SYSTEM OPS NORMAL. (M)

Part: CLAMPS — LOOSE (APU)

ON TAKEOFF TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. AMBIENT TEMP WAS 82 F AND APU HAD BEEN OFF FOR 10 MIN. RAN T/O POWER W/13TH STAGE BLEED ON. FOUND LOOSE CLAMPS ABOVE AND BELOW AIR CONDITIONING PRESSURE REGULATOR AND OUTBOARD CLAMP AT AVERAGE VALVE. TIGHTENED AND SECURED CLAMPS. PROBLEM CORRECTED IAW DC-9MM 36-20-0. (M)

Part: TEMP SENSOR — FAILED (APU)

DTW - FLT 566 - ON T/O, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. AMBIENT TEMP WAS 68 DEGREES F, AND APU HAD BEEN OFF FOR 10 MINUTES. SUSPECT BLEED AIR LEAK. REMOVED AND REPLACED TAIL COMPARTMENT TEMP SENSORS. OPS CHECK NORMAL IAW MM CHAPTER 36-20-2. (M)

Part: BRAKE ASSY — LOCKED UP (NR 4 MAIN)

FLL - FLT 205 - PARKING BRAKES WOULD NOT RELEASE FOR PUSH-BACK. AIRCRAFT NOT MOVEABLE. FOUND NR 4 MAIN BRAKE ASSY LOCKED-UP. REMOVED AND REPLACED SAME IAW DC-9 MM 32-42-1. LEAK CHECK GOOD. (M)

Part: BRAKE FUSE — FAILED (RT MLG)

RSW - FLT 621 - RIGHT BRAKE PEDAL DOES NOT ACTIVATE BRAKING FROM EITHER SIDE OF COCKPIT. REMOVED AND REPLACED ALL RT BRAKE FUSE ASSEMBLY IAW DC-9 MM CHAPTER 32-42-6. OPS CHECK GOOD. REFERENCE GTIA9700250.

Part: BRAKE FUSE — FAILED (RT MLG)

RSW - FLT 621 - RIGHT BRAKE PEDAL DOES NOT ACTIVATE BRAKING FROM EITHER SIDE OF COCKPIT. REMOVED AND REPLACED ALL RT BRAKE FUSE ASSEMBLY IAW DC-9 MM CHAPTER 32-42-6. OPS CHECK GOOD. REFERENCE GTIA9700250.

Part: BRAKE FUSE — FAILED (RT MLG)

RSW - FLT 621 - RIGHT BRAKE PEDAL DOES NOT ACTIVATE BRAKING FROM EITHER SIDE OF COCKPIT. REMOVED AND REPLACED ALL RT BRAKE FUSE ASSEMBLY IAW DC-9 MM CHAPTER 32-42-6. OPS CHECK GOOD. REFERENCE GTIA9700250.

Part: BRAKE FUSE — FAILED (RT MLG)

RSW - FLT 621 - RIGHT BRAKE PEDAL DOES NOT ACTIVATE BRAKING FROM EITHER SIDE OF COCKPIT. REMOVED AND REPLACED ALL RT BRAKE FUSE ASSEMBLY IAW DC-9 MM CHAPTER 32-42-6. OPS CHECK GOOD. (M)

Part: CONNECTOR — DIRTY (LAV SMOKE DET)

DTW - FLT 621 - LEFT LAVATORY SMOKE DETECTOR CAME ON. NO SMOKE OR HEAT IN LAVATORY. REMOVED CONNECTOR, CLEANED PINS AND OPS CHECKED IAW MM CHAPTER 26-10-8. (M)

Part: TRIM MECHANISM — OUT OF ADJUST (RUDDER)

DTW - RUDDER TRIM INDICATOR SHOWS 6 UNITS LEFT WITH TRIM TAB CENTERED. ADJUSTED RUDDER CONTROL TRIM MECHANISM IAW MM CHAPTER 27-10-7. OPS CHECK GOOD. (M)

Part: THROW LIMITER — OUT OF ADJUST (RUDDER)

DTW - RUDDER PEDAL MOVEMENT NOT RESTRICTED WHEN FLAP RUDDER STOP ENGAGED. ADJUSTED RUDDER PEDAL MOVEMENT AND AUX RUDDER THROW LIMITER, RUDDER STOP SWITCH AND FLAP RUDDER POSITION SWITCH. OPS CHECK GOOD IAW DC-9 MM 27-40-14. (M)

Part: CLAMP — LOOSE (LT ACM)

RSW - FLT 621 - AFT COMPARTMENT TEMP HIGH LIGHT AFTER TAKEOFF. MASTER WARNING CONTINUED TO FLICKER, TEMP HIGH LIGHT ON AND OFF CONTINUOUSLY. TIGHTENED LOOSE CLAMP ON LEFT ACM. AIRCRAFT OPS CHECK GOOD ON GROUND IAW DC-9 MM 36-20-2. (M)

Part: SWITCH — OUT OF ADJUST (RT MLG DOOR)

RSW - FLT 621 - RIGHT GEAR UNSAFE AND GEAR DOOR OPEN LIGHT CAME ON AFTER TAKEOFF. FOLLOWED FCOM. RIGHT GEAR UNSAFE AND GEAR DOOR OPEN LIGHT ON DUE TO OPEN LIGHT OUT OF ADJUSTMENT. ADJUSTED MAIN GEAR INBOARD DOOR POS SWITCH IAW DC-9 MM 32-60. (M)

Part: INTERCOSTAL — CRACKED (BS 180)

MHV - FORWARD ACCESSORY COMPARTMENT AT STATION 180 ABOVE LONGERON L-29 AND INTERCOSTAL IS CRACKED. FABRICATED AND REPLACED INTERCOSTAL PER SRM 51-10-3, 51-30-2. (M)

Part: SKIN — MIS REPAIRED (BS 996)

MHV - FS 996 - BELOW LONGERON 18R, REPAIR INSTALLED WITH BLIND FASTENERS, DOES NOT MEET REQUIREMENTS OF SRM 53-01 FIG 2, SHEET 3. REMOVED AND REPLACED REPAIR DOUBLER AND FILLER FABRICATED, TREATED, FINISHED, FASTENERS INSTALLED AND SEALED PER SRM 51-01, 51-10-3, 51-20-0, 51-30-8. (M)

Part: REAR SPAR — DAMAGED (WS 164)

MHV - PERFORM REPAIR AT WING STATION XRS 164 RT REAR SPAR PER DRAWING 5060165. REMOVED TEMP REPAIR, INSPECTED, STOPPED DRILLED CRACKS AND REINSTALLED TEMP REPAIR IAW SRM 51-10-3, 51-10-33, 51-30-5, 51-10-2, SB A47-146, AND DRAWING J06027. (M)

Part: FRAME — CORRODED (BS 889)

MHV - FRAME HAS CORROSION AT STATION 889 RBL 63 BELOW WINDOW ZF 4-12 AND 30. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND REPAIRED FRAME PER SRM 51-10-3, 51-10-3, 53-019, 51-10-5, 1-2. (M)

Part: SKIN — CORRODED (CARGO COMPT)

MHV - AFT FUSELAGE RT CARGO DOOR BETWEEN PRESSURE SEAL AND DOOR PAN AT LOWER AREA OF DOOR HAS EXTENSIVE EXFOLIATION CORROSION. REMOVED AND REPLACED OUTER DOOR PANE IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-7, 51-30-5. (M)

Part: TRIM TAB — CORRODED (LT ELEVATOR)

MHV - LEFT GEARED TAB HAS HONEYCOMB DAMAGE AND DELAMINATION. REPAIRED IAW SRM 55-04 PAGE 3 AND 51-70-2 PAGE 80. (M)

Part: FRAME — TORN (BS 148)

MHV - RIGHT SIDE OF COCKPIT AT FUSELAGE STATION 148 55 INCHES ABOVE FLOOR LEVEL INBOARD FLANGE OF FRAME TORN AND MISSING A 1 INCH BY 2.25 INCH SECTION. REMOVED DAMAGED AREA IAW SRM 53-03 FIG 4. FABRICATED DOUBLER AIND INSTALLED PER SRM 51-10-3, 53-03 FIG 4. (M)

Part: FLOOR — CORRODED (COCKPIT)

MHV - COCKPIT FLOOR RIGHT SIDE, SMALL PAN AREA UNDER GALLEY NR 1 HAS EXFOLIATION CORROSION AT STATION 160. REMOVED DAMAGED AREA, FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1. (M)

Part: PANEL — BROKEN (LT WING)

MHV - LEFT LOWER WING PANEL NR 2114 INTERLOCK STRIP LOWER UNDERSIDE OF PANEL BROKEN. REMOVED DOUBLER, FABRICATED DOUBLER PER SRM 51-10-2. INSTALLED PER SRM 51-10-3, 51-30-2. (M)

Part: PANEL — BROKEN (LT WING)

MHV - LEFT LOWER WING PANEL NR 2114 INTERLOCK STRIP LOWER UNDERSIDE OF PANEL BROKEN. REMOVED DOUBLER, FABRICATED DOUBLER PER SRM 51-10-2. INSTALLED PER SRM 51-10-3, 51-30-2. (M)

Part: SKIN — CORRODED (RT WING)

MHV - RT WING UPPER SKIN TO AFT SPAR END CAP HAS BULGING AND CORROSION EMITTING AT LOWER SURFACE XRS 152. TWO INCH SQUARE AREA APPROXIMATELY. REMOVED CORROSION, TRIM AND BLENDED AREA IAW EA 5730-96-001, PER SRM 51-20-0, 51-30-2, 51-30-8, 57-09 FIG 12. (M)

Part: STIFFENER — CRACKED (LT WING/FUS)

MHV - LEFT WING TO FUSELAGE FILLET FAIRING STIFFENER IS CRACKED. REMOVED OLD STIFFENER, FABRICATED NEW STIFFENER PER SRM 53-50-0, FABRICATED PATCH PER SRM 55-01 INSTALLED PER SRM 51-30-3. (M)

Part: TAILCONE — DELAMINATED (AFT FUSELAGE)

FIBERGLASS REPAIR ON LEFT INSIDE OF TAILCONE IS DELAMINATION. REPAIRED DELAMINATION PER SRM 51-90-0. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

MHV - RIB AND SKIN IN THRESHOLD LIGHTING HOLE BAY AT THE BASE OF FRONT OF AFT CARGO DOOR IS CORRODED, EXFOLIATING IN SEVERAL LOCATIONS. REMOVED DAMAGE INTERCOSTAL AND INSTALLED NEW PART IAW SRM 51-30-2, 51-10-3, 53-10-1. (M)

Part: SKIN — DAMAGED (R1 DOOR)

MHV - R-1 DOOR LOWER EDGE OF DOOR BENT, DELAMINATING, AND DEFLECTED INWARD. REPAIRED PER SRM 52-03 PAGE 1. (M)

Part: TAB — PUNCTURED (LT ELEVATOR)

MHV - LEFT ELEVATOR CONTROL TAB HAS A HOLE PUNCTURED IN IT. REMOVED DAMAGED AREA PER SRM 55-04 REPAIRED PER SRM 55-22-0 PAGE 10, FIG 6, SRM 55-04. (M)

Part: BULKHEAD BRACKET — BROKEN (AFT BULKHEAD)

MHV - AFT CARGO CENTERLINE BOTTOM OF AFT BULKHEAD AT CARGO FLOOR BRACKET BROKEN. FABRICATED BRACKET PER SRM 51-10-1. REMOVED BROKEN BRACKET AND INSTALLED NEW PER SRM 51-30-02. (M)

Part: JAMB — MISREPAIRED (CARGO DOOR)

MHV - AFT CARGO DOOR JAMB AFT LOWER REPAIR NOT PER DOUGLAS DRAWING SR0953117. REMOVED REPAIR, FABRICATED DOUBLERS AND FILLER PER SRM 53-05, INSTALLED IAW SRM 53-10-3, 51-30-05. (M)

Part: DOOR FRAME — CRACKED (BS 916)

MHV - AFT FUSELAGE FRAME FOR CARGO DOOR HAS CRACKS, LOWER DOUBLER STATION 916. FABRICATED DOUBLER AND FILLER PER SRM 53-10-1, TRIMMED SKIN PER EA 5330-96-005, INSTALLED PER SRM 51-30-5. (M)

Part: FRAME — CORRODED (BS 148)

MHV - COCKPIT RIGHT SIDE FRAME AT STATION 148 C/T FLOOR HAS EXFOLIATION. REMOVED DAMAGE SECTION OF FRAME. FABRICATED FRAME SECTION AND DOUBLERS PER EA 5310-96-004 AND SRM 51-10-2 INSTALLED IAW 51-30-2, 51-10-3. (M)

Part: CHAF STRIP — WORN (RT WING)

MHV - RT WING FORWARD FLAP LEADING CHAF STRIP HAS A HOLE CHAFED THROUGH. FABRICATED PER SRM 51-10-2. INSTALLED IAW SRM 51-10-3, 51-30-2. (M)

Part: BULKHEAD ANGLE — CORRODED (AFT BULKHEAD)

MHV - AFT BULKHEAD RIB ANGLE, AFT PIT RBL 40 AREA CORRODED CAUSING DELAMINATION. ALSO, CORROSION RBL 20 TO 45. CORRODED RIB ANGLE. REMOVED AND REPLACED RIB ANGLE IAW SRM 51-01, 51-30-2. (M)

Part: FLOOR — CRACKED (BS 200)

MHV - FLOOR STRUCTURE, 3 INCH CRACK ON FLOOR WEB AT STATION 200 RBL 43 ZF-1. FABRICATED WEB IAW 51-10-1. REMOVED AND REPLACED WEB IAW 51-10-3, 51-30-2. (M)

Part: SKIN — CORRODED (BS 940-965)

MHV - AFT CARGO PIT RIGHT SIDE BETWEEN STRINGER 27 AND 29R FS 940-965 HAS 4 AREAS OF CORROSION THAT EXCEED LIMITS ON FUSELAGE SKIN. REMOVED CORROSION AND FABRICATED DOUBLER PER SRM 53-04. INSTALLED PER EA 5330-96-0005 SRM 53-10-3. (M)

Part: FLOOR — CRACKED (BS 218)

MHV - TWO INCH CRACK ON FLOOR WEB STATION 218 RBL 43 ZF 1. REMOVED CRACKED FLOOR WEB, FABRICATED NEW FLOOR WEB IAW 53-10-1, INSTALLED IAW 51-10-3, 51-30-2. (M)

Part: SKIN — CORRODED (BS 996)

EVIDENCE OF CORROSION AT LAP SPLICE STATION 996 LONGERON 26R. OPENED SKIN LAP, REMOVED CORROSION, FABRICATED FILLER AND INSTALLED IAW 53-10-3, 53-04, 53-01. (M)

Part: FLOOR — CORRODED (BS 237)

MHV - FLOOR STRUCTURE HAS POPPED RIVET AT STATION 237 RBL 54 ZF1. C/T WEB HAS TWO BOLTS MISSING/CORRODED AT STATION 200 RBL 43 AND 45 ZF1. WHILE REPAIRING FASTENERS THE WEB AND GUSSET WERE FOUND TO BE CORRODED BEYOND LIMITS. REMOVED DAMAGED AREAS, FABRICATED NEW WEB AND GUSSETT IAW 51-10-2 INSTALLED IAW 51-30-1, 51-30-3. (M)

Part: SEAT TRACK — CORRODED (BS 200-237)

MHV - OUTBOARD SEAT TRACK RIGHT SIDE AT STATION 200-237 IS CORRODED BEYOND LIMITS. FABRICATED NEW SEAT CHANNEL FROM EXISTING SEAT TRACK MATERIAL INSTALLED SEAT TRACK IAW 53-05 FIG 4A-1 PAGE 8E. (M)

Part: FRAME — CRACKED (BS 192)

MHV - FUSELAGE FRAME FOR SERVICE DOOR HAS A CRACK AT STATION 192 PASSED .1875 HOLE AT LOWER DOUBLER. FABRICATED DOUBLER, FILLER, INSTALLED IAW SRM 53-05 FIG 35 CLASS 1 REPAIR. (M)

Part: JAMB — CRACKED (PAX DOOR)

FORWARD PASSENGER ENTRANCE DOOR JAMB UPPER FORWARD CORNER IS CRACKED ADJACENT TO 2ND FASTENER DOWN FROM RUB BAR. ALSO, PREVIOUS REPAIR IS NOT TO SRM (53-05-FIG 26). CRACK NOT CUTOUT AND FILLER MISSING. DISASSEMBLED AREA CUTOUT CRACK PER SRM 53-05 FIG 26 NOTE 6. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER SRM 53-05, FIG 26, 51-10-3. (M)

Part: BULKHEAD DOOR — CRACKED (AFT PRESS BLKHD)

MHV - AFT PRESSURE BULKHEAD DOOR EXTERIOR SKIN HAS DEEP GOUGE AROUND ARC OF DOOR HANDLE. REPLACE AFT PRESSURE BULKHEAD DOOR EXTERIOR SKIN IAW 51-30-2, 51-10-3, 52-10-02. (M)

Part: STRINGER — CORRODED (FUSELAGE)

MHV - LEFT FLOOR STRINGER IN AFT PIT WHERE IT JOINS RIB FROM MIDDLE OF CARGO DOOR HAS CORROSION WITH EXFOLIATION UNDERNEATH. FABRICATED TWO CHANNEL AND SPLICES PER C0137. OK TO INSTALL AND INSTALLED COMPLETE PER SRM 51-30-02. ALODINED AND PRIMED AS NECESSARY PER 51-10-03. (M)

Part: BRACKET — CRACKED (PAX DOOR)

FORWARD ENTRY DOOR TOP AFT CORNER ATTACH BRACKET CRACKED. FABRICATED NEW BRACKET, DRILLED AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-30-1. (M)

Part: SUPPORT — CRACKED (BS 237)

MHV - FLOOR SUPPORT HAS A 1 INCH CRACK AT STATION 237 LBL 2 ZFO. REMOVED LEFT FLOOR SUPPORT FABRICATED NEW SUPPORT AND INSTALLED IAW 51-10-3, 53-10-2, 51-30-2. (M)

Part: ANGLE — BROKEN (BS 775)

MHV - A/C FUSELAGE LEFT WING FILLET SUPPORT ANGLE AT FS 775 LOWER END IS BROKE OFF AND AT STATION 718 IS CRACKED RT SIDE AT STATION 718 AND 756 IS CRACKED. FABRICATED SUPPORTS IAW SRM 53-53-0 INSTALLED IAW 51-30-2. (M)

Part: SUPPORT — CRACKED (BS 237)

MHV - FLOOR SUPPORT HAS 1.5 INCH CRACK AT STATION 237 RBL 2 ZFO. REMOVED RT FLOOR SUPPORT. FABRICATED NEW SUPPORT AND INSTALLED PER SRM 53-10-2, 53-10-3. (M)

Part: DOOR — CORRODED (LAV SERVICE)

MHV - AFT LAVATORY SERVICE PANEL, LEFT SIDE OF A/C, HAS EXFOLIATION CORROSION. REMOVED AND REPLACED AFT LAVATORY SERVICE DOOR IAW MM 38-30-0. INSTALLED COMPLETE, TRIMMED TO FIT ALODINED, AND PRIMED IAW SRM 51-10-3. (M)

Part: STRUCTURE — CORRODED (BS 598-550)

MHV - FWD CARGO COMPT FROM FS 598 TO FS 550 LONGERONS 28 LT, 29 LT, 30 CENTER, AND 29 RT, ATTACH ANGLES, SPLICE PLATE, AND INTERIOR SKIN CORRODED. REMOVED SURFACE CORROSION (IN LIMITS). ALODINE AND PRIMED AREA IAW SRM 51-10-3. LONGERON AND SPLICE INSULATION TRANS TO JOB C00029. REINSTALLED AIR DUCT AND RESAFETIED WIRE PER MM 28-189-0. CORROSION ON SKIN OF .065, REMOVED .002 MATERIAL IN LIMITS PER 53-01. CORROSION ON STRUCTURE OF .175, REMOVED .002 MATERIAL IN LIMITS PER 53-01. NEW REPAIR COMPLETED WITH EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER AS PER SRM 53-04 PAGE 35 FIG 12B. (M)

Part: SEAT TRACK — CORRODED (BS 200-230)

MHV - FORWARD CABIN SEAT TRACK AT RBL 22 FS 200 THROUGH 230 AT STATION 200 HAS CRACKS, DRILL START AND CORROSION. REMOVED OLD SENT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK IAW 51-10-3, 51-10-2 AND 53-05. (M)

Part: SKIN — MIS INSTALLED (BS 600)

MHV - STATION 600 LONGERON 30 SKIN REPAIR NOT PER SRM 53-04 FIG 12B. FINGER DOUBLERS NOT INSTALLED. INSTALLED FINGER DOUBLERS AS PER SRM 53-04 PAGE 35 FIG 12B. (M)

Part: FITTING — CORRODED (CARGO DOOR)

MHV - AFT CARGO DOOR AFT EDGE GUIDE FITTINGS AND FASTENERS CORRODED. AFT DOOR EDGE SPACER CORRODED. BEAM 5 UPPER FORWARD ATTACH ANGLE, 1 FASTENER CORRODED. REMOVED AND REPLACED GUIDE FITTINGS PER SRM'S 52-30-4 AND 20-31. REMOVED CORROSION WITHIN LIMITS PER SRM 52-01 PAGE 5 (.002 MATERIAL REMOVED). REMOVED AND REPLACED FASTENER PER SRM 51-30-5. (M)

Part: ANGLE — CRACKED (BS 150)

MHV - COCKPIT OVERHEAD, FORWARD TOP MOUNT OF EPC LBL 12.5 ANGLE IS CRACKED FS 150. REPLACED NEW BRACKET IAW 53-01-0, 20-16-0. (M)

Part: MOUNT — CORRODED (NR 1 ENGINE)

MHV - NR 1 ENGINE AFT MOUNT FILLING HAS SURFACE CORROSION. REMOVED AND REPLACED NR 1 AFT VIBRATION ISOLATOR IAW 71-20-2. (M)

Part: SUPPORT — CORRODED (BS 148-168)

FLOOR SUPPORT ANGLE RT SIDE STATION 148-168 HAS EXFOLIATION CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA FLOOR SUPPORT ANGLES, FABRICATE DOUBLERS AND FILLERS IAW SRM 53-01 FIG 2. INSTALLED IAW 51-30-2. (M)

Part: RIB — CRACKED (VERT STAB)

MHV - VERTICAL STABILIZER LE PANEL RT SIDE HAS 5 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. LEFT SIDE HAS 3 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. FABRICATED AND INSTALLED PARTS IAW 55-02 FIG 14, 51-10-3, 51-20-0, 51-30-0. ALL CRACKS STOP DRILLED. (M)

Part: PANEL — CRACKED (LT TE FLAP)

MHV - LEFT WING LOWER FLAP AREA NR L-2 BUTTE PANEL HAS A LARGE CRACK. REPAIRED HONEY COMB PANEL PER SRM 57-04, DOUBLER INSTALLED PER SRM 57-04 AND 57-30. (M)

Part: DOOR BEAM — CRACKED (CARGO DOOR)

MHV - AFT CARGO DOOR BEAM NR 1 AFT ATTACH ANGLE CRACKED. REPAIR PER SRM 51-10-4, 51-30-5, 51-30-1 (NEW PART INSTALLED). (M)

Part: FLOOR PANEL — PEELING (CABIN)

MHV - FLOOR PANEL NR 5 MYLAR PEEING, DOUBLER MISSING ON BOTH SIDES AND HAS SOME AREA DELAMINATING. FABRICATED AND INSTALLED (3) NEW DOUBLERS. REBOND DOUBLERS PER MM 20-20-0. (M)

Part: FRAME — CORRODED (BS 929)

MHV - FRAME HAS CORROSION AT STATION 929 RBL 62 ZF 6-15. REMOVED CORRODED AREA, FABRICATED NEW SUPPORT BRACKET PER SRM 53-11-3. INSTALLED IAW 51-30-1. (M)

Part: SKIN — CRACKED (BS 69.55)

MHV - DURING NDT INSPECTION OF AIRCRAFT PER SID 53.09.029 CRACKS WERE INDICATED IN THE FUSELAGE SKIN AT 5 RIVETS AT FS 69.550 APPROXIMATELY 15 INCH LEFT OF CENTERLINE OF THE AIRCRAFT. INSPECTED FOUND INITIAL REPAIR PER DRAWING SR09530239 WAS IMPROPERLY INSTALLED. RE-REPAIR ACCOMPLISHED PER SRM 53-04 FIG 12B. (M)

Part: SUPPORT — CRACKED (BS 389)

MHV - FORWARD CARGO UPPER FLOORBEAM TO SKIN FORWARD SUPPORT IS CRACKED AT STATION 389 RBL 60 2F-6. INSTALLED NEW BRACKET PER SRM 51-30-3. (M)

Part: ANGLE — CRACKED (BS 180)

MHV - FORWARD ACCESSORY COMP AT STATION 180 AT CENTER LINE ABOVE LONGERON 30 ATTACH ANGLE FOR FLOOR SUPPORT IS CRACKED, ALSO ATTACH ANGLE ABOVE 29L IS ALSO CRACKED. FABRICATED ANGLES. REMOVED AND REPLACED ANGLES PER SRM 51-10-02, 51-10-3, AND 51-30-02. (M)

Part: FLOORBOARD — CRACKED (CABIN)

MHV - FLOORBOARD NR 21 HAT SECTIONS CHAFED, CRACKED AND BROKEN OUT. REPAIRED FLOORBOARD IAW 53-05, INSTALLED IAW 51-30-2. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

MHV - AFT FLOOR PANEL S/N 2686 AND END DELAMINATED ALONG EDGE AND CRACKED IN LOWER ANGLE ALONG DELAMINATION. REPAIRED DELAMINATION PER SRM 53-05. STOP DRILLED CRACK PER SRM 53-01 AND REPAIRED PER SRM 53-05. FABRICATED REPAIR DOUBLERS PER SRM 53-05. ALODINED AND PRIMED PER SRM 51-10-3. INSTALLED REPAIR DOUBLERS PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL NR 21 HAS 6 CRACKS IN HAT CHANNELS. REMOVED DAMAGED AREAS, FABRICATED DOUBLERS AND INSTALLED IAW SRM 53-05, 51-10-3, 51-10-4, 53-30-2. (M)

Part: PAN — CRACKED (PAX DOOR)

MHV - PASSENGER ENTRY DOOR PAN FORWARD LOWER CORNER ON FORWARD SIDE IN CRACK JUST BELOW LOWER HINGE. REMOVED AND REPLACED DOOR PAN SEGMENT PER SRM 52-05, 51-10-3, 51-10-4, 51-30-2, 51-30-5, 51-30-7. (M)

Part: STRUCTURE — DAMAGED (FUSELAGE)

MHV - FLOOR BOARD, WINGS BOX AREA, UPPER AREA HAS SEVERAL CRACKS AND TORN OUT HOLES. HAT CHANNELS HAVE CRACKS AT THE FORWARD ENDS, INSULATION TAPE IS LOOSE. FLOOR SKIN DAMAGED BEYOND REPAIR. REMOVED FLOORBOARD PANEL SKIN AND FABRICATED NEW PANEL SKIN. REMOVED DAMAGED HAT SECTIONS. FABRICATED 3 HAT SECTIONS AND 3 HAT SECTION DOUBLERS. ALODINED AND PRIMED HAT SECTIONS AND SKIN PANEL PER SRM 51-10-3 REPAIRED FLOORBOARD IAW 53-05 FIG 1. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-8. INSTALLED NEW INSULATION PER MM 25-22-0. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL HAS BREAK OUT FROM ONE FASTENER HOLE ALONG EDGE AND TWO EACH EDGE STRIPS MISSING. FABRICATED PATCH IAW SRM 55-01. TREATED AND PRIMED PATCH IAW SRM 51-10-03. INSTALLED PATCH WITH RIVETS IAW SRM 51-30-2. FABRICATED EDGE STRIPS IAW MM 53-20-1. INSTALLED AND BONDED WITH SCOTCH GRIP IAW MM 20-20-0. (M)

Part: SPRING — BROKEN (ATTEND SEAT)

MHV - FLIGHT ATTENDANT SEAT, AFT CABIN, RETURN SPRING RIGHT SEAT HINGE IS BROKEN. LUBRICATED HINGE SPRING, INSTALLED RETURN SPRING SENT FULLY RETRACTS IAW 25-23-21. (M)

Part: BULKHEAD FRAME — CRACKED (AFT PRESS BLKHD)

MHV - AFT PRESS BULKHEAD LEFT SIDE, THE 1ST AND 2ND HORIZONTAL FRAMES UP FROM CABIN FLOOR LEVEL ARE CRACKED. STOP DRILLED CRACKS. FABRICATED DOUBLER AND CLIPS PER SRM 51-01. INSTALLED PER 53-01 FIG 2, 51-10-3. (M)

Part: ENGINE MOUNT — CORRODED (NR 2 ENGINE)

MHV - NR 2 ENGINE PYLON AFT MOUNT HAS SURFACE CORROSION ON OUTER SURFACE. REMOVED AND REPLACED NR 2 ENGINE AFT VIBRATION ISOLATER AND LINK IAW 71-20-2. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL AFT CABIN 15A IS CRACKED ON TOP SURFACE AND ONE HAT CHANNEL IS CRACKED ALONG SAME EDGE. ALSO, AT OPPOSITE END OF WHERE CRACKS ARE INSULATION BATTING UNBONDING AND PROTRUDING BEYOND EDGE. FABRICATED AND INSTALLED HAT CHANNEL REPAIRS (2) PER SRM 53-05 FIG 1. REPAIR SKIN CRACKS BY STOP DRILLING. FABRICATE AND INSTALL PATCH REPAIR PER SRM 55-01 PAGE 7. REPAIR INSULATION BATTING PER MM 25-22-0. (M)

Part: FLOOR PANEL — CRACKED (LAVATORY)

MHV - LAVATORY FLOOR PANEL NR 8 HAS A CRACK ON RIGHT AFT CORNER, FORWARD SIDE HAS 4 FASTENER HEAD BROKEN. STOP DRILLED CRACK, FABRICATED DOUBLER, INSTALLED DOUBLER IAW 53-01, 53-05, 51-10-3, 51-30-3. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL NR 17 HAS CRACK AT FORWARD SIDE CENTER BESIDES SCREW HOLES. INSTALLED SKIN DOUBLER IAW 55-01 FIG 2. (M)

Part: FLOOR PANEL — TORN (CABIN)

MHV - FLOOR PANEL AFT CABIN FASTENER HOLE IS TORN OUT AT CORNER. REPAIRED BY FABRICATING RD DOUBLER. ALODINE AND PRIMED PER SRM 51-10-3 AND DRILLED AND COUNTERSUNK PER SRM 51-10-4 AND INSTALLED RIVETS PER SRM 51-30-2. REPAIRED PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

MHV - FLOOR PANEL NR 1 HAS DOUBLER DELAMINATION ON SOME AREAS, MYLAR CRACK ON 3 AREAS, DELAMINATED HAT SECTION, NUMEROUS CRACKS IN HAT SECTIONS AND CORROSION. REBONDED PER 53-20-21. DRILLED TACK RIVETS PER 51-10-4. INSTALLED RIVETS PER 51-30-3. TREATED CORROSION PER SRM 51-10-3. ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED HAT SECTIONS PER SRM 53-05 FIG 1. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL NR 13, LEFT FORWARD CORNER HAS CRACK. STOP DRILLED CRACK AND BONDED DOUBLER IAW 53-20-1. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

MHV - AFT FLOOR PANEL, 1 CORNER IS DELAMINATING AND INSULATION IS MISSING. THERE IS A HOLE IN THE SKIN. FABRICATED A PATCH FOR THE DAMAGE. ALODINED AND PRIMED PATCH IAW SRM 51-10-3. INSTALLED PATCH IAW SRM 51-30-2. INSTALLED RIVETS IN DELAMINATING CORNER IAW SRM 51-30-2. INSTALLED INSULATION IAW MM 25-22-0, PAGE 201. (M)

Part: HAT CHANNEL — CRACKED (FUSELAGE)

MHV - PANEL NR 24, HAT CHANNEL AT AFT END OF PANEL HAS CRACKED OUT FASTENER HOLE. REPAIRED HAT CHANNEL IAW SRM 53-05, 51-10-3. (M)

Part: FLOORBOARD — BROKEN (WING BOX AREA)

MHV - FLOORBOARD WING BOX AREA, ON CORNER, METAL SECTION BROKEN OUT, INSULATION BATTING MISSING ALONG BOTH LONG EDGES, ONE SHORT EDGE HAS UNBONDING, AND OTHER SECTIONS OF SEAL MISSING. REMOVED BROKE SECTION FROM CORNER OF FLOORBOARD FABRICATED FILLER AND DOUBLER ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED FLOORBOARD PER SRM 53-05, FIG 1. INSTALLED FASTENERS PER SRM 57-30-2. INSTALLED INSULATION PER MM 25-22-0. REBONDED GILLINER PER MM 53-20-1. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

MHV - NR 4 FLOOR PANEL HAS DELAMINATING DOUBLER AND SOME AREAS MISSING, ONE CRACKED SCREW HOLE, INSULATION MISSING AND MYLAR BROKEN. REPAIRED DELAMINATING DOUBLER AND INSTALLED MISSING DOUBLERS PER MM 53-20-1. REPAIRED CRACKED SCREW HOLE PER SRM 53-05 AND 53-01. FABRICATED REPAIR DOUBLER AND INSTALLED PER 53-05. INSTALLED MISSING INSULATION AND REPAIRED BROKEN MYLAR PER MM 25-22-0. ALODINED AND PRIMED PER SRM 51-10-3. (M)

Part: STEP — CORRODED (VENTRAL STAIR)

MHV - AFT VENTRAL STAIR. RETRACTABLE STEP HAS CORROSION. REMOVED AND REPLACED STEP IAW 51-30-8. (M)

Part: FLOOR PANEL — DAMAGED (CABIN)

MHV - FLOOR PANEL, AFT CABIN, UPPER SURFACE HAS HOLES, RIVETS PULLED THROUGH AND CRACKS, LOWER SURFACE HAS CRACKS TO FASTENERS, PROTRUDING UPSET HEADS SHOULD BE FLUSH AND INSULATION TAPE IS LOOSE. REPAIRED HOLE PER SRM 53-05 BY INSTALLING DOUBLER. ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED RIVET BY REMOVING AND REPLACING RIVETS PER SRM 51-30-2. REPAIRED CRACK TO FASTENERS BY INSTALLING DOUBLER PER SRM 53-05, DRILLED AND COUNTERSUNK HOLES PER SRM 51-10-4 AND INSTALLED PER SRM 51-30-2. REMOVED RIVET UPSET AND TOUCH COUNTERSUNK AND REINSTALLED RIVETS DOUBLER FLUSH PER SRM 51-30-2. REPAIRED INSULATION AND LOOSE TAPE PER MM 25-22-0. (M)

Part: FLOOR PANEL — MISSING (CABIN)

MHV - LEFT OUTBOARD FLOOR PANEL HAS DOUBLER MISSING SOME AREAS DELAMINATING, TWO EACH, SPACER MISSING AT END OF U-CHANNEL. REPLACED MISSING SPACERS AT END OF U-CHANNEL. REBOND DOUBLER PER MM 53-20-1. FABRICATE AND INSTALL NEW DOUBLER PER SRM 53-20-0, FIG 3C SPACERS CEMENTED PER MM 20-20-0. (M)

Part: FLOOR PANEL — BROKEN (CABIN)

MHV - FLOOR PANEL 12 HAT CHANNEL SECTION AT ONE END HAS BROKEN OUT ABOUT 1 INCH LONG. OTHER SECTION HAS DEEP GOUGE. REPAIRED PER 53-21-0. INSTALLED RIVETS PER 51-30-2. BLENDED GOUGE EPR 53-01, REMOVED .008 FROM .040 MATERIAL, WITHIN LIMITS PER SRM 53-01, TREATED AND PRIMED PER 51-10-3. (M)

Part: FLOOR PANEL — CORRODED (CABIN)

MHV - FLOOR PANEL NR 16 FORWARD HAS LIGHT CORROSION BETWEEN DOUBLER AND FORWARD END OF PANEL, ALSO, CRACK FROM FASTENER TO OUTSIDE OF PANEL. INSIDE IS MISSING INSULATION AND HAS LOOSE TAPE. BLENDED CORROSION (.002 REMOVED PER 51-10-3, WITHIN LIMITS PER 51-10-1). FABRICATED AND INSTALLED DOUBLER PER 55-01, FIGURE 2. INSTALLED INSULATION (3 EACH) PER MM 25-22-0. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

MHV - RIGHT FORWARD OUTBOARD WING BOX FLOOR PANEL HAS DELAMINATING DOUBLERS, TWO SECTION DOUBLERS MISSING (TWO EACH) SPACERS MISSING AT END OF U-CHANNEL. REPLACE MISSING SPACERS AT END OF U-CHANNEL. REBOND DOUBLER PER MM 53-20-1. FABRICATED AND INSTALLED NEW DOUBLERS PER SRM 53-20-0 FIG 3C. SPACERS CEMENTED PER MM 20-20-0. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL 14 FORWARD, ONE CORNER IS CRACKED ABOUT 2 INCHES LONG AND INSULATION BATTING MISSING ALONG ONE EDGE AND OPPOSITE BATTING IS COMING APART. REPAIRED CORNER PER SRM 55-01, FIG 2. TREATED AND PRIMED PER 51-10-3. INSTALLED FASTENERS PER 51-30-2. INSTALLED INSULATION PER MM 25-22-0. (M)

Part: FLOOR PANEL — DEFORMED (CABIN)

MHV - FLOOR PANEL NR 13, FORWARD END OF PANEL IS DEFORMED, RT HAT CHANNEL IS DELAMINATED AT CTR OF PANEL AND DEFORMED AT AFT END. FOUR CORNERS ARE DELAMINATED AND INSULATION IS MISSING. REPAIR HAT CHANNEL DELAMINATION PER SRM 51-30-3. STRAIGHTEN PANEL DAMAGE PER SRM 53-01. REPAIR DOUBLERS ON FOUR CORNERS PER MM 53-20-1 (INSULATION IS NOT REQUIRED IN ELECTRICAL POWER CABLE PANELS REF MM 25-27-0). (M)

Part: PANEL — CRACKED (LT WING)

MHV - LEFT WING PANEL 1508 HAS A CRACK THAT EXISTS FROM RIVET HOLE TO CAM-LOCK HOLE. REMOVED CRACK, FABRICATED ANGLE, INSTALLED IAW SRM 57-22-3, 51-30-0. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

MHV - NR 23B FLOOR PANEL IS DELAMINATING AT CORNERS. INSULATION TAPE IS LOOSE. REBONDED FLOOR PANELS AT CORNERS WITH SCOTCH GRIP ADHESIVE PER MM 53-20-1 AND RETAPED INSULATION PER MM 25-22-0. (M)

Part: BULKHEAD — CRACKED (BS 218)

MHV - ON BULKHEAD BETWEEN FORWARD CARGO BAY AND FORWARD ACCESSORY COMPARTMENT AT STATION 218 EXISTS SEVERAL CRACK REPAIRS THAT ARE NOT PER SRM. REMOVED EXISTING REPAIRS, FABRICATED NEW PATCHES PER SRM 53-10-1 FIG 7B, 53-01 FIG 2, 51-10-3. INSTALLED IAW 53-01 FIG 2. (M)

Part: PANEL — CRACKED (LT WING)

MHV - LEFT WING UNDER AILERON CAM-LOCK RECEPTACLE AT INBOARD END OF PANEL 1509 EXISTS A CRACK FORWARD AND AFT OF FASTENER HOLE. REMOVED CRACK, FABRICATED NEW ANGLE PER SRM 57-22-3 INSTALLED IAW 51-30-0. (M)

Part: FLOOR BOARD — TORN (BS 218-237)

MHV - LEFT FUSELAGE FLOOR MEMBRANE THAT ATTACHES TO OUTBOARD SEAT TRACK AT STATION 218-237 LBL 44 IS TORN ON FORWARD SIDE. REMOVED OLD MEMBRANE, FABRICATED NEW MEMBRANE AND INSTALLED PER SRM 51-30-01, 51-10-3. (M)

Part: FLOOR BOARD — CORRODED (BS 237)

MHV - LEFT FS 237 LBL 44, FLOOR MEMBRANE HAS A CRACK FORWARD OUTBOARD EDGE CORROSION AROUND FITTING AT STATION 237 THAT ATTACHES TO MEMBRANE. CLEANED CORROSION FROM FITTING, REMOVED DAMAGED AREA FABRICATED DOUBLER AND INSTALLED IAW 51-10-3, 51-01-01, 51-10-2, 53-10-2. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - NR 19 FLOOR PANEL, CORNER DELAMINATING, INSULATION MISSING CENTER AREAS OF HAT CHANNELS DELAMINATING, SKIN TORN AT CORNER. REPAIRED FLOORBOARD PER SRM 53-05. FABRICATED REPAIR DOUBLER PER SRM 53-5. ALODINED AND PRIMED PER 51-10-3. INSTALLED REPAIR DOUBLER PER SRM 53-05. STOP DRILLED TEAR IN TOP OF SKIN PER SRM 53-01. REPAIRED HAT CHANNELS PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL NR 15 HAS NUMEROUS CRACKS AND DELAMINATION. REMOVED DAMAGED AREA, FABRICATED NEW HAT CHANNELS PER SRM 53-05 FIG 1, INSTALLED IAW 51-30-2, 51-30-7. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

MHV - AFT FLOOR PANEL HAS DELAMINATING DOUBLERS RIVETS PULLED OUT OF HAT CHANNELS AND TEARS IN TOP SKIN OF PANEL. REPAIRED FLOOR BOARD PER SRM 53-05. FABRICATED SKIN REPAIR DOUBLERS PER SRM 53-05. ALODINED AND PRIMED PER SRM 51-10-3. STOP DRILLED TEAR IN TOP SKIN PER SRM 53-01. REPAIRED GRILLINER DOUBLERS PER MM 53-20-1. ALSO, REPLACED SPACER FOR FASTENER INSTALLATION PER SRM 53-05. (M)

Part: BULKHEAD FRAME — CRACKED (AFT PRESS BLKHD)

MHV - AFT PRESSURE BULKHEAD RIGHT SIDE, 1ST 2ND, 3RD HORIZONTAL BULKHEAD FRAMES UP FROM CABIN FLOOR LEVEL ARE CRACKED. STOP DRILLED CRACKS, FABRICATED DOUBLERS AND INSTALL IAW 53-01 FIG 2. (M)

Part: BULKHEAD FRAME — CRACKED (AFT PRESS BLKHD)

MHV - AFT PRESSURE BULKHEAD RT SIDE 4TH HORIZONTAL BULKHEAD FRAME UP FROM CABIN FLOOR PANEL IS CRACKED AT OUTBOARD END. STOP DRILLED CRACK, FABRICATED DOUBLERS AND INSTALLED IAW 51-10-2, 51-10-3, 53-01 FIG 2. (M)

Part: FLOOR PANEL — CRACKED (CABIN)

MHV - FLOOR PANEL NR 10 FORWARD HAS 3 HAT SECTIONS WITH CRACKS IN CORNERS (2 AT 1 END AND ONE AT THE OTHER END). ALSO, INSULATION BATTING FALLING APART. REPAIRED HAT SECTIONS IAW SRM 53-05, ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED INSULATION PER MM 25-22-0. (M)

Part: LONGERON — CORRODED (FUSELAGE)

MHV - SURFACE CORROSION WITH EXFOLIATION ON LONGERON DIRECTLY BENEATH OUTFLOW VALVE IN AFT PIT, RIB ANGLE IN FRONT OF OUTFLOW VALVE HAS SURFACE CORROSION DOWN AND TO RT OF VALVE. REMOVED CORRODED STRAP, FABRICATED NEW PART ALODINED, PRIMED, AND INSTALLED IAW SRM 51-10-1, 51-10-3, 51-30-4. REMOVED CORROSION PER SRM 51-10-3 (WAS .040, IS .039, WITHIN LIMITS PER SRM 53-01 FIG 1. ALODINED AND PRIMED PER SRM 51-10-3. (M)

Part: DOOR — CRACKED (PAX COMPT)

MHV - PASSENGER ENTRY DOOR NUMEROUS CRACKS. REPAIR DOOR IAW 52-05, 51-30-2, 51-30-5. (M)

Part: FRAME — CORRODED (FUSELAGE)

MHV - SURFACE CORROSION ON FORWARD SIDE OF FRAME 1ST IN FRONT OF AFT PIT AFT BULKHEAD BETWEEN LONGERON 30 AND 29. FABRICATED NEW SECTION OF RIB AND FILLER. REMOVED CORROSION OFF OF FRAME THAT WAS WITHIN LIMITS. REMOVED 2.70 BY 80 SECTION OF FRAME THAT WAS OUT OF LIMITS. ALODINED AND PRIMED FRAME AND FABRICATED PARTS. INSTALLED FABRICATED PARTS PER SRM 53-01 FIG 1, 51-10-3, 53-04 PAG 191, 51-30-2, AND 51-30-5. (M)

Part: STRINGER — CORRODED (CARGO DOOR)

MHV - NUMEROUS PATCHES OF SURFACE CORROSION ALONG TOP OF RIGHT STRINGER FORWARD OF AFT CARGO DOOR TO FORWARD BULKHEAD OF AFT PIT. SECTION CLOSEST TO CARGO DOR IS DELAMINATING. REMOVED BOTH ENDS, FABRICATED AND INSTALLED (2) SPLICES AND (2) ENDS IAW SRM 53-02. REMOVED CORROSION FROM CHANNEL IAW SRM 51-10-3 (.0005 REMOVED WITHIN LIMITS). ALODINED AND PRIMED AREAS IAW SRM 51-10-3. INSTALLED CHANNEL COMPLETE IAW SRM 51-30-2. (M)

Part: FLOOR PANEL — DAMAGED (BS 117)

MHV - COCKPIT FLOOR AT STATION 117 RBL 3 INCH FROM CENTER LINE EXISTS DENTS AND A CRACK .823 INCH LONG THROUGH SUB STRUCTURE BARRIER FLOOR AND PLASTIC CABLE SHROUD. REMOVED DAMAGED AREA, FABRICATED AND INSTALL DOUBLERS PER SRM 53-01 FIG 2, 51-10-03, 51-30-02, 51-20-0. (M)

Part: FLOOR PANEL — DAMAGED (CABIN)

NR 30 FLOOR PANEL HAS 3 CRACKS. REMOVED DAMAGED MATERIAL, DOT LOCATION 24, 25, 26 AND FABRICATED FILLERS AND DOUBLERS. ALODINED AND PRIMED PER SRM 51-10-3. DRILLED AND COUNTERSUNK PER SRM 51-10-4. INSTALLED RIVETS PER SRM 51-30-3. REPAIRED PER SRM 53-05, PAGE3. (M)

Part: FLOOR PANEL — DAMAGED (BS 142)

MHV - COCKPIT FLOOR AT STATION 142 RBL 17 INCH FROM CENTERLINE EXISTS A HOLE .275 INCH DIAMETER THROUGH SUB STRUCTURE BARRIER FLOOR. REMOVED DAMAGE AREA AND FABRICATED AND INSTALLED NEW PARTS IAW SRM 53-01 FIG 2, 51-30-02. (M)

Part: AIR STAIR — MIS REPAIRED (AFT FUSELAGE)

MHV - PERFORM REPAIR PER DOUGLAS SERVICE REWORK DRAWING SR09530219 (STAIR DOOR AREA). REMOVED TEMP REPAIR, FABRICATED NEW DOUBLERS AND FILLER IAW SRM 53-05-17A. INSTALLED PER DRAWINGS SR09530031 AND SR09530219. (M)

Part: ANGLE — CORRODED (BS 217)

MHV - FORWARD ACC COMP, FLOOR SUPPORT ANGLE AT FS STATION 217 HAS SEVERAL CORRODED CLIPNUTS AND LIGHT CORROSION ON BOTTOM SIDE. REMOVED AND REPLACED ANGLE AND CLIPNUTS IAW SRM 51-30-2, 51-30-8. (M)

Part: FRAME — CORRODED (BS 945)

MHV - FRAME HAS CORROSION AT STATION 945 RBL 61 AND 63 AF1 AND 3. FABRICATED AND INSTALLED NEW WEB IAW 51-10-2 AND 51-30-0. (M)

Part: FLOOR — CORRODED (BS 902/908)

MHV - FLOOR WEB HAS CORROSION AT STATION 902 RBL 59 ZF1 AND STATION 908 RBL 59 HAS EVIDENCE OF CORROSION BETWEEN WEBS. FABRICATED AND REPLACED CORRODED WEB IAW 51-10-3/51-30-0. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

MHV - FLOOR PANEL NR 2A HAS SEVERAL SMALL CRACKS AT THE END ROW OF RIVET HOLES. STOP DRILLED HOLE AND ADDED DOUBLER IAW 51-10-3, SRM 51-10-4. (M)

Part: FLOOR — CORRODED (BS 931-948)

MHV - FLOOR WEB HAS CORROSION ON STATION 931-948 RBL 59 ZF1. REMOVED DAMAGE, FABRICATED NEW WEB AND INSTALLED IAW 51-10-2, 51-10-3, 51-30-0. (M)

Part: ANGLE — CORRODED (BS 237)

MHV - FLOOR SUPPORT REPAIR HAS CORROSION AT STATION 218 BL 0 ZF-1 AND STATION 237 BL 0 ZF-1. REMOVED AND REPLACED CORRODED ANGLES, NEW ANGLES WERE FABRICATED AND INSTALLED IAW 51-30-2, 51-10-3, 51-10-4, 51-30-0, AND 53-03 FIG 3. (M)

Part: STRUCTURE — DAMAGED (FUSELAGE)

MHV - FLOORBOARD 27, 3 HAT SECTIONS CRACKED AT ONE END AND 2 SECTIONS CRACKED AT OTHER END. INSULATION BATTING MISSING ON ONE END, FALLING APART ON THE OTHER, AND UNBONDED AND FALLING APART AT A FEW AREAS IN THE CENTER SECTION. REMOVED 5 CRACKED HAT SECTIONS, DURING REWORK FOUND 4 SKIN CRACKS. FABRICATED 5 HAT SECTIONS, 5 HAT SECTION DOUBLERS, 2 FILLERS AND 3 DOUBLERS. ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED PER SRM 53-05, FIG 1. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-8. REBONDED BATTING PER MM 25-22-0. (M)

Part: BULKHEAD FRAME — CRACKED (AFT PRESS BLKHD)

MHV - AFT PRESSURE BULKHEAD DOOR CANTED FRAME ON RT SIDE OF DOOR FRAME IS CRACKED AT UPPER END WHERE THE BULKHEAD MEETS THE FUSELAGE SKIN. REMOVED FRAME, TRIM CRACK AREA PER SRM 51-01, DYE PEN, NO CRACKS FOUND. REINSTALLED FRAME IAW SRM 51-10-3, 53-11-3 PAGE 16D. (M)

Part: JAMB — DAMAGED (CARGO COMPT)

MHV - AFT CARGO PIT, LOWER FORWARD CORNER OF DOOR JAMB HAS DAMAGE ON EDGE OF DOUBLER AND IS DELAMINATING AND HAS NUMEROUS DAMAGED FASTENERS. FABRICATED DOUBLER AND INSTALLED WITH SRM 51-10-2 AND 51-10-3. (M)

Part: CHANNEL — CRACKED (LT MLG DOOR)

MHV - LEFT OUTBOARD GEAR DOOR U-CHANNEL AT AFT SURFACE OF DOOR IS CRACKED. REMOVED OLD PART FABRICATED AND INSTALLED NEW PART IAW 52-10-2, 52-80-0. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

MHV - FLOOR PANEL AFT CABIN HAS TWO CRACKS IN AFT AREA OF SKIN. CUT OUT CRACKS AND FABRICATED FILLER AND DOUBLER PER SRM 51-10-2. ALODINED PER SRM 51-10-3. DRILLED AND COUNTERSUNK PER SRM 51-10-4. INSTALLED FASTENERS PER SRM 51-30-2. FLOOR PANEL REPAIR COMPLETED PER SRM 53-21-0. (M)

Part: TIE CLIP — CRACKED (BS 965)

MHV - PYLON SHEAR WEB TO LONGERON 17R, TIE CLIP IS CRACKED IN TWO, STATION 965. REPLACED TIE CLIP PER SRM 51-10-1, 51-10-3, 51-30-2. (M)

Part: BULKHEAD FRAME — CRACKED (AFT PRESS BLKHD)

MHV - AFT PRESS BULKHEAD FORWARD SIDE LEFT CANTED FRAME ABOVE BULKHEAD DOOR HAS A CRACKED ATTACH CLIP AT UPPER END WHERE BULKHEAD MEETS THE FUSELAGE SKIN. REMOVED AND FABRICATED NEW CLIP, INSTALLED IAW 51-10-2, 51-10-3, 53-01. (M)

Part: BRACKETS — CRACKED (WS 250/256)

MHV - RIGHT WING LEADING EDGE WING STATION XRS 250 AND XRS 256 HAVE CRACKED MOUNTS. REMOVED OLD BRACKETS, FABRICATED IAW 51-10-2 AND INSTALLED IAW 51-10-1/3. (M)

Part: MEMBRANE — CRACKED (BS 950)

MHV - CRACK IN MEMBRANE AT FS 950 48 INCHES LEFT OF A/C C/T. FABRICATED AND INSTALLED DOUBLERS IAW 53-01, PAGE 17, 51-10-3. (M)

Part: JAMB DOUBLER — MISSING (CARGO DOOR)

MHV - FORWARD CARGO DOOR JAMB FORWARD SIDE REPAIR IS NOT PER DOUGLAS DRAWING SR09530117. FINGER DOUBLER MISSING. FABRICATED FILLERS AND DOUBLERS PER 51-10-2 AND EA 5330-96-001 REWORK DONE IAW EA 5330-96-001 AND SRM 51-30, 51-10-3. (M)

Part: FLOOR — CRACKED (BS 970)

MHV - FLOOR WEB HAS A 4 INCH CRACK BETWEEN 2 CUTOUTS AT STATION 970 LBL 50. FABRICATED DOUBLERS PER SRM 53-01, FIG 7. INSTALLED IAW SRM 51-10-3. (M)

Part: FLOOR — MISINSTALLED (CABIN)

MHV - PASSENGER CABIN FLOOR MEMBRANE REQUIRES MODIFICATION PER DOUGLAS REWORK DRAWING SR09530002. MODIFIED FLOOR MEMBRANE PER DOUGLAS DRAWING SR09530002 FS 718-737 AND 737-756 LT AND RIGHT SIDES INBOARD OF FUSELAGE SKIN. (M)

Part: CHANNEL — CRACKED (BS 1601)

MHV - FORWARD CABIN RIGHT FS 1601 CHANNEL HAS A HOLE IN IT WITH A CRACK EMANATING OUTBOARD .5 INCH. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-01, 51-10-03. (M)

Part: FLOOR — WORN (BS 218)

MHV - FLOOR WEB HAS TWO WEAR AREAS 1 INCH LONG OVER 50 PERCENT OF MATERIAL THICKNESS AT STATION 218 LBL 4 AND 7 ZF1. CUT OUT DAMAGE AREA FABRICATED FILLERS AND DOUBLER INSTALLED IAW 53-01, 51-30-2. (M)

Part: FLOOR BOARD — CRACKED (FUSELAGE)

MHV - FLOOR BOARD, WING BOX AREA, THREE CRACKS IN TOP SKIN AREA, INSULATION TAPE IS LOOSE. CUT OUT CRACKED AREA ON FLOOR BOARD, FABRICATED FILLER AND DOUBLER AND REPAIRED PER SRM 53-05, FIG 1. ALODINED AND PRIMED PER SRM 51-10-3. INSTALLED RIVETS PER SRM 51-30-2. RETAPED INSULATION PER MM 25-22-0. (M)

Part: LONGERON — CORRODED (FUSELAGE)

MHV - LONGERON IN 3RD LEFT SIDE BAY FOR AFT BULKHEAD OF AFT PIT IS CORRODED HAS ABOUT 8 INCHES SECTION OF EXFOLIATION. FABRICATED, TREATED, FINISHED, AND INSTALLED A NEW STIFFENER PER THE FOLLOWING SRM'S 51-10-0, 51-10-3, AND 51-30-4. (M)

Part: TRAP PANEL — CRACKED (BS 697)

MHV - LEFT TRAPEZOIDAL PANEL UPPER ATTACH LEG LOCATED AT PREVIOUS REPAIR CUT OUT C/T WING ATTACH ANGLE STATION 697 LBL 592 F-12 CRACK .80 INCH LONG. REMOVED NOTED CRACK TO THE FOURTH HOLE IAW SRM 57-9, FIG 6, NOTES 1 AND 2 AND 51-10-3. (M)

Part: FLOOR BOARD — CRACKED (CABIN)

MHV - CABIN FLOOR BOARD HAS A CRACK IN UPPER SKIN. REPAIRED PER SRM 53-05, FIG 1. CUT OUT CRACKED AREA AND FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30-2. (M)

Part: CHANNELS — CRACKED (COCKPIT)

MHV - FLOOR PANEL RIGHT COCKPIT HAS CHANNELS DEFORMED, CRACKED AND WITH RIVETS PULLING THROUGH. REMOVED AND REPLACED CRACKED HAT CHANNEL PER SRM 53-05, FIG 1. FABRICATED REPLACEMENT HAT SECTION. ALODINED AND PRIMED PER SRM 51-10-3. REPLACED FASTENERS PER SRM 51-30-2 AND 51-30-8. (M)

Part: FLOOR — CRACKED (COCKPIT)

MHV - COCKPIT FLOOR AREA LEFT STORAGE AREA HAS A CRACK DEVELOPING IN FORWARD TOP EDGE OF RETAINER. FABRICATED AND INSTALLED DOUBLER, CRACK STOP DRILLED IAW 52-01, 51-01, 51-10-03. (M)

Part: FLOORBEAM — CRACKED (BS 389/408)

MHV - FORWARD CARGO COMPARTMENT FLOORBEAM LOWER LIP BL0 BROKEN OFF AT FS 389 AND FLOORBEAM LOWER LIP AT FS 408 IS CHAFED. REMOVED DAMAGED AREA, FABRICATED FLAT DOUBLERS AND ANGLE DOUBLERS AND INSTALLED IAW 53-10-8. (M)

Part: FLOOR PANEL — CRACKED (BS 200-237)

MHV - FORWARD LAVATORY FLOOR PANEL FS 200 TO 237 HAS SEVERAL FASTENER HOLES WITH CRACKS AND SURFACE CORROSION AROUND SCREW HOLES. REMOVED AND REPLACED SKIN AND DOUBLERS IAW 51-10-0, 51-10-2, 51-10-3, 51-10-4 AND 51-30-3. (M)

Part: STIFFENER — CRACKED (CABIN)

MHV - FLOORBOARD NR 6 FOR FORWARD CABIN HAS A STIFFENER CRACKED. REPAIRED HAT SECTION IAW 53-05 FIG 1, 51-10-3, 51-30-2, 51-30-8. (M)

Part: FLOOR PANEL — DELAMINATED (BS 699-737)

MHV - RIGHT FLOOR PANEL STATION 699-737 DOUBLER DELAMINATION ON SOME AREA. REATTACHED PER MM 53-20-1. REBONDED FIBERGLASS PER MM 53-20-1. (M)

Part: FLOOR — CORRODED (BS 820-830)

MHV - SURFACE CORROSION ON FLOOR WEB AT STATION 820-830 RBL 59 ZF1. REMOVED DAMAGE AREA, FABRICATED NEW WEB. INSTALLED IAW 53-05, 51-10-3. (M)

Part: FLOOR PANEL — CORRODED (LAVATORY)

MHV - FORWARD LAV FLOOR PANEL HAS SURFACE CORROSION AND NUMEROUS RIVET HEADS. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER INSTALLED IAW 51-10-3, 53-05 FIG 1, 51-30-2. (M)

Part: ANGLE — LOOSE RIVETS (BS 598)

MHV - RIGHT WING FUSELAGE STATION 598, UPPER WING ATTACH ANGLE HAS LOOSE RIVETS C/T NUTPLATE. FORMED AND INSTALLED NEW DOUBLER IAW 53-01, FIGURE 2. (M)

Part: DOUBLER — CRACKED (NLG DOOR)

MHV - REPAIR ON NOSE GEAR LT HINGED DOOR EXTERNAL REPAIR NEEDS INSPECTION TO VERIFY COMPLIANCE WITH SRM 53-05 FIG 62. STOP DRILLED CRACK, FABRICATED NEW DOUBLER, INSTALLED IAW 53-05 FIG 62. (M)

Part: FLOOR PANEL — CRACKED (BS 200-237)

MHV - FORWARD CABIN FLOOR PANEL RBL 20 TO 43 FS 200 TO 237 HAS DENT WITH CRACKS AND UNDER SIDE HAS A CRACK ON PANEL STRINGER. REPAIRED FLOOR PANEL IAW SRM 53-01, FIG 2 SRM 53-05 FIG 1, 51-10-03. (M)

Part: STIFFENER — CRACKED (NR 1 ENGINE COWL)

MHV - NR 1 ENGINE NOSE COWL HAS A STIFFENER WITH A DAMAGED AND CRACKED FLANGE AT AFT EDGE OF COWL. REMOVED OLD STIFFENER AND FABRICATED AND INSTALLED NEW STIFFENER IAW 51-01-01 AND 51-02-01. (M)

Part: DOUBLERS — NOT INSTALLED (BS 332)

MHV - STATION 332 LONGERON 30 REPAIR ON ANTENNA IS MISSING FINGER DOUBLERS BOTH SIDES. REMOVED OLD DOUBLER, FABRICATED INTERNAL DOUBLER AND EXTERNAL DOUBLER IAW SRM 53-04, INSTALLED PARTS SRM 51-30-2, 51-30-5, 53-04. (M)

Part: FLOOR PANEL — CRACKED (BS 160-198)

MHV - FORWARD CABIN FLOOR PANEL INBOARD OF L1 DOOR FS 160 TO 198 HAS A HOLE WITH A CRACK NEXT TO COCKPIT DOOR CUTOUT, LIGHT CORROSION LEVEL 1. FABRICATED REPAIR IAW SRM 51-21-0, FIG 1. REPAIRED PANEL IAW SRM 53-05, 51-10-3. (M)

Part: DOUBLER — NOT INSTALLED (E/E DOOR)

MHV - REPAIR AFT OF E/E DOOR AT STATION 257 NOT IN COMPLIANCE WITH SRM 53-04, FIG 12B. NO FINGER DOUBLER INSTALLED. INSTALLED NEW FINGER DOUBLER PER SRM 53-04, FIG 12B. (M)

Part: JAMB — CORRODED (SERVICE DOOR)

MHV - FORWARD CABIN R-1 SERVICE DOOR LOWER THRESHOLD HAS EXFOLIATION CORROSION INSIDE. REMOVED SURFACE CORROSION. FOUND TO BE WITHIN LIMITS PER SRM 51-10-3 (FS 150-FS 237). (M)

Part: PACK — SMOKING (CABIN)

AFTER LANDING AND BLOCK IN RSW. APPEARS TO HAVE A TRACE OF SMOKE IN CABIN AREA WITH PACK OPERATING. INSPECTED AND OPERATED BOTH LEFT AND RIGHT PACKS USING RIGHT PACK IN NORMAL. ALL OPERATIONS AND INDICATIONS ARE NORMAL, IAW CHAP 21. NO SMOKE IN CABIN NOTED. (M)

Part: BATTERIES — LOW VOLTAGE (CABIN)

ON DAILY INSPECTION, FOUND LEFT OVERWING EXIT LIGHTING INOP. RECHARGED EMERGENCY LIGHTING POWER SUPPLY BATTERIES. SYSTEM OPERATIONAL CHECKS GOOD. (M)

Part: EPR INDICATOR — INOPERATIVE (NR 2 ENGINE)

NR 2 EPR INOP. CLEARED MOISTURE FROM PT2 AND PT7 LINES AND FOUND NR 2 EPR GAUGE INOP. REMOVED AND REPLACED EPR GAUGE. SYSTEM OPS CHECK GOOD. (M)

Part: EPR TRANSMITTER — MALFUNCTIONED (NR 2 ENGINE)

RIGHT EPR GAUGE WOULD NOT POWER WHEN SPOOLING THE ENGINES UPON TAKING THE RUNWAY FOR TAKEOFF. REMOVED AND REPLACED RIGHT EPR TRANSMITTER. SYSTEM OPS CHECK GOOD. (M)

Part: EEL POWRE SUPPLY — INOP (CABIN)

FORWARD EMERGENCY LIGHT POWER SUPPLY INOP. REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT POWER SUPPLY. (Z)