N791AL

Part: COMPRESSOR — STALLED (NR 3 ENGINE) · airframe 66,325 hrs · 19,563 cycles

REJECTED TAKEOFF AT 60 KTS DUE COMPRESSOR STALL NR 3 ENGINE. INSPECTED ENGINE INLET AND EXAUST, NO DEFECTS FOUND. ENGINE RUN UP C/W IN ACCORDANCE WITH MM 71-00. UNABLE TO DUPLICATE PROBLEM. OK FOR SERVICE.

Part: ENGINE — VIBRATION (NR 2) · airframe 66,241 hrs · 19,529 cycles

NR 2 ENGINE HUMMING NOISE CHANGING IN PITCH DIRECTLY PROPORTIONAL TO VIBRATION IN THROTTLE, ALL OTHER PARAMETERS NORMAL, POWER RETARDED TO IDLE, HUMMING & VIBRATION STOPPED. REMOVED AND REPLACED NR 2 ENGINE PER JOB CARD DC8-UM-003. OPERATIONAL CHECK ON ENGINE RUN NORMAL.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 66,082 hrs · 19,474 cycles

AT TOP OF DESCENT 08:23 ZULU, SHUT DOWN NR 2 ENGINE DUE TO OIL PRESS LIGHT ON AND OIL PRESS 30 PSI WITH ENGINE AT IDLE. WINDMILLING OIL PRESS 11 PSI N1 26.5 PERCENT. SECURED NR 2 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH GMM 6-3-4 AND 6-3-5. COMPLETED RED BORDER NR 18470. REMOVED NR 2 ENGINE S/N 671323 DUE TO OIL PRESSURE LOSS AND INSTALLED ENGINE S/N P-671360 IN ACCORDANCE WITH ARROW AIR JOB CARD NR DC8UN-O03. OPERATIONAL AND LEAK CHECK AT ENGINE RUN-UP IN ACCORDANCE WITH ARROW AIR JOB CARD NR DC8UN-093 AND DC8 MM 74-00; FOUND NORMAL, NO LEAKS NOTED.

Part: ENGINE — LEAKING (NR 4) · airframe 66,007 hrs · 19,443 cycles

DURING CLIMBOUT OF MGGT NOTICED NR 4 ENGINE LOSS OF OIL QUANTITY, OIL PRESSURE AND LIGHT. PROCEEDED TO SHUTDOWN ENGINE ACCORDING TO CHECKLIST. REMOVED AND REPLACED ENGINE NR 4 S/N 669510, AND INSTALLED ENGINE S/N P671066 IN ACCORDANCE WITH ARROW AIR JOB CARD DC8UN-003. ADJUSTMENT AND TEST NR 4 ENGINE IN ACCORDANCE WITH DC-8 MM 71-00; FOUND NORMAL PARAMETER.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 66,702 hrs · 19,720 cycles

DURING CRUISE LOST HYDRAULIC QUANTITY TO STAND PIPE. PERFORMED EMERGENCY/ABNORMAL CHECK LIST. FOUND ONE HYDRAULIC LINE, ENGINE NR 3, TO ENGINE LINE OPERATIONAL CHECK AND LEAK CHECK OK IN ACCORDANCE WITH MM 29-00-00.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 64,950 hrs · 19,021 cycles

AFTER TAKEOFF OUT OF KMIA VENT DOOR WARNING LIGHT CAME ON & CABIN PRESS WAS UNABLE TO BE MAINTAINED.

Part: WHEEL — SHEARED (MLG) · airframe 64,845 hrs · 18,978 cycles

ON POST-FLIGHT FOUND NR 3 MAIN WHEEL SHEARED OFF. REMOVED AND REPLACED NR 3 MAIN WHEEL ASSEMBLY IAW MM 32-40-1. ALSO, REMOVED AND REPLACED NR 4 MAIN WHEEL ASSEMBLY IAW MM 32-40-1.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 64,454 hrs · 18,821 cycles

GEAR NOT LATCHED; LIGHT ILLUMINATED AFTER GEAR UP. FOLLOWED ABNORMAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED PROXIMITY SWITCH BOX SYSTEM BITE TEST NORMAL AND OPERATIONAL CHECK NORMAL WITH GEAR SWING IAW MM 32-60-0.

Part: PROXIMITY SWITCH — DIRTY (MLG) · airframe 64,387 hrs · 18,789 cycles

GEAR NOT LATCHED LIGHT CAME ON IN FLIGHT AND STAYED ON ALL THE TIME. LUBED UPLATCHED MAIN & NOSE GEAR MECHANISM IAW MM 12-81-1; CLEANED ALL PROXIMITY SWITCHES IAW MM 20-50-1. OPERATIONAL CHECK FOUND NORMAL IAW MM 32-30-0. SEVERAL GEAR SWING PERFORMED.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 64,229 hrs · 18,723 cycles

NR 1 ENGINE COMPRESSOR STALLED, REDUCED POWER 1.50 EPR, N1 TACH FLUX AND MAX "O". OIL TEMP INCREASING. ENGINE SHUT DOWN 05:30Z WINDMILLING OIL PRESSURE 16 PSI. NOTE: PRELIMINARY INSPECTION REVEAL C1 BEARING FAILURE. CORRECTIVE ACTION:

Part: ARM — BROKEN (NLG DOOR) · airframe 64,047 hrs · 18,678 cycles

AFTER GEAR RETRACTION NOISE AND VIBRATION FROM NOSE GEAR AREA. POST FLIGHT INSPECTION FOUND GEAR DOOR ARM BROKEN WITH DAMAGE TO FUSELAGE AT DOOR HINGE AREA. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER REPAIR IAW DC8 SRM 53-2-1 FIG 7 PAGE 111. REMOVED AND REPLACED ROD ON NOSE LANDING GEAR (NLG) FIX DOOR LT SIDE IAW DC8 MM 32-30-0 PAGE 201.

Part: CARGO TRACK — BROKEN (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK, THE FOLLOWING WAS FOUND; MAIN CARGO DOOR COMPARTMENT STA 420, LBL 50 TRACK WITH BREAKAGE. CUT AWAY DAMAGED SECTION OF TRACK IAW DC8 SRM 53-2-3, PREPARED A NEW SECTION OF TRACK AND FABRICATED SPLICES IAW DC8 SRM 53-2-3, PRIMED PARTS IAW DC8 SRM 51-1-8, INSTALLED PARTS IAW DC8 SRM 53-2-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK THE FOLLOWING WAS FOUND; FS 1606 AFT PRESSURE BULKHEAD TEE CAP WITH 8 INCH CRACK BTW L-9L AND L12L. CUT LONGERONS 11L, 12L AND 13L AND REMOVED SPLICES (OPEN), CUT DAMAGED AREA OF FRAME IAW DC8 SRM 53-2-0, PREPARED NEW FRAME SEGMENT IAW BOEING ATM. TREATED AND PRIMED REPAIR AREA AND PARTS IAW DC8 SRM 51-1-8, INSTALLED FRAME SEGMENT AND REINSTALLED SPLICES (4 EACH) IAW DC8 SRM 53-2-0, FABRICATED LONG SPLICES (3 EACH) IAW DC8 SRM 53-2-2, TREATED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED LONG SEGMENT AND SPLICES IAW SRM 53-2-0.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT DOOR JAMB UPPER WEB BROKEN STA 360, L-6L. CUT OUT DAMAGED AREA IAW DC8 SRM 53-2-0, FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-0, PRIMED FILLER AND DOUBLER IAW DC8 SRM 51-1-8 AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-0.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W UPPER SURFACE WITH 0.750 INCH CRACK, STA 934. DRILLED A STOP HOLE AT END OF CRACK IAW DC8 SRM 53-2-0, FABRICATED DOUBLER IAW DC8 SRM 53-2-0, PRIMED DOUBLER IAW DC8 SRM 51-1-8 AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STA 1280, BTW L29R AND L31R SKIN WITH NICKS. TRIMMED OUT DAMAGE AREA IAW AS ELEVEN INC DRAWING AS11490 SHEET 1 OF 2 AND 2 OF 2, DATED 02/19/03; FABRICATED FILLER, DOUBLER AND TRIPLER IAW AS ELEVEN INC DRAWING AS11490 SHEET 1 OF 2 AND 2 OF 2, DATED 02/19/03; TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8, AND INSTALLED PARTS IAW AS ELEVEN INC DRAWING AS11490 SHEET 1 OF 2 AND 2 OF 2, DATED 02/19/03.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA 740, RBL 45, TRACK WITH CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3, CUT AWAY DAMAGED SECTION OF TRACK AND FABRICATED SPLICES IAW DC8 SRM 53-2-3, PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW DC8 SRM 53-2-3.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND, AFT LOWER CARGO COMPARTMENT STA 1280, FLOOR PANEL ANGLES (02 EACH) CRACKED. REMOVED ANGLES IAW DC8 SRM 51-1-21, FABRICATED NEW ANGLES IAW DC8 SRM 51-1-4, PRIMED NEW ANGLES IAW DC8 SRM 51-1-8 AND INSTALLED NEW ANGLES IAW DC8 SRM 51-1-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK, THE FOLLOWING WAS FOUND, RADOME BULKHEAD WEB LOWER SECTION WITH CRACKS, STA 44. CUT OUT DAMAGED AREA, FABRICATED STRAP AND FILLER IAW DC8 SRM 53-2-0, PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW DC8 SRM 53-2-0.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,899 hrs · 18,628 cycles

DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR W/W STA 857 AND XCW51 PRESSURE BULKHEAD STIFFENER UPPER SECTION ANGLE WITH CRACK. DRILLED A STOP HOLE AT END OF CRACK IAW DC8 SRM 53-2-0, FABRICATED REINFORCEMENT IAW DC8 SRM 53-2-0, PRIMED REINFORCEMENT IAW DC8 SRM 51-1-8 AND INSTALLED REINFORCEMENT IAW DC8 SRM 51-1-21.

Part: LANDING GEAR — COLLAPSED (NLG) · airframe 63,895 hrs · 18,626 cycles

EMERGENCY TURNBACK DUE TO NOSE GEAR MALFUNCTION. ON ROLLOUT NOSE GEAR COLLAPSED AT 70 KTS. EMERGENCY UNITS APPLIED FOAM FIRE PROTECTION ON RUNWAY AND PURPLE DRY CHEMICAL WAS USED IN COCKPIT AREA PRECAUTIONARY.

Part: THRUST REVERSER — WORN (NR 1 ENGINE)

MHLM - FLT 541 - ON POST FLIGHT, FOUND NR 1 ENGINE LOWER REVERSER TRACK DAMAGED. TROUBLESHOT AND FOUND THAT THE LOWER TRACK FORWARD YOKE ASSY EYEBOLT SEPARATED FROM ENGINE CASE ATTACH POINT. NO OTHER DAMAGE TO THE ENGINE. REMOVED AND REPLACED LOWER TRACK AND YOKE ASSY OPS NORMAL IAW MM 78-30-00. (M)

Part: EGT INDICATOR — MALFUNCTIONED (NR 4 ENGINE)

MIA - FLT 628 - AIR TURNBACK. DURING CLIMB, NR 4 ENGINE INDICATED 40 DEGREES LOWER THAN OTHER ENGINES, HOWEVER, WHEN LEVELED OFF AND AFTER SETTING CRUISE POWER, EGT CONTINUED DECREASING UNTIL IT INDICATED 100 DEGREES CELSIUS LOWER THAN OTHER ENGINES. PERFORMED PRECAUTIONARY SHUT DOWN AT THAT TIME (1202 Z) WINDMILLING OIL PRESSURE WAS 43 PSI. DUMPED 23,000 POUNDS OF FUEL AND RETURNED TO MIAMI WITHOUT INCIDENT. REPAIRED COLD SOLDER JOINT AT OUTER END OF BALANCE RESISTOR SPOOL. ALSO, REPLACED EGT INDICATOR AS PRECAUTIONARY. PERFORMED ENGINE RUN-UP. ALL PARAMETERS CHECKED NORMAL IAW DC8 MM 77-20-0 AND 71-00-00. (X)

Part: VALVE — LEAKING (LT COCKPIT)

MIA - FLT 9038 - DURING CLIMB, F/O'S AIRSPEED INDICATOR WAS SHOWING 10 KTS LOWER THAN THE CAPT AND THE DIFFERENCE INCREASED WITH THE ALTITUDE UP TO 50 KTS LOWER FL230. SELECTED F/O'S STATIC SELECTOR TO ALT FOR LANDING. REMOVED AND REPLACED KNOB ALT PITOT SELECTOR VALVE. PERFORMED OPS CHECK PITOT STATIC SYSTEM. FIRST OFFICER AND ALTERNATE, FOUND NORMAL IAW MM 34-12-0. (M)

Part: INDICATOR — MALFUNCTIONED (COCKPIT HSI)

MIA - FLT 617 - CAPTAINS COURSE BAR WILL STAY CENTERED WITHIN 25 DEGREES OF COURSE. REPLACED CAPTAINS HSI INDICATOR, OPS NORMAL IAW MM 34-52-0. (M)

Part: MECHANISM — OUT OF ADJUST (MLG DOOR)

MIA - FLT 941 - AIR TURNBACK - AFTER DEPARTURE GEAR UPLATCH CHECK RESULTED IN 'DOORS NOT LATCHED' LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST WITH SAME RESULTS. THE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION. LETTER ON DURING DESCENT THE 'GEAR NOT LATCHED' LIGHT ALSO ILLUMINATED. PERFORMED ADJUSTMENT OF GEAR DOOR FOLLOWUP MECHANISM. OPS CHECKED NORMAL IAW DC-8 MM 32-31-5. (M)

Part: TORQUE TUBE — CRACKED (RT MLG)

MIA - FLT 940 - AFTER LANDING AND DURING TAXI, THE RIGHT MAIN LANDING GEAR GREEN LIGHT WAS OUT INTERMITTENTLY AND THE RED GEAR DOOR UNSAFE RED LIGHTS ILLUMINATED, SUSPECTED FAULTY GEAR DOWN MICROSWITCH. FOUND RT MLG 'A' FRAME WITH CRACKED LUG. REMOVED AND REPLACED MLG 'A' FRAME ASSY (TORQUE TUBE) AND LINKAGE, OPS CHECKED NORMAL ON GEAR SWING IAW DC-8 MM 32-11-3 AND MM 32-30-3. (M)

Part: WARNING LIGHT — ILLUMINATED (GEN OVERLOAD)

ON TAXI, GENERATOR OVERLOAD LIGHT ILLUMINATED. ACCOMPLISHED OK LIST, LIGHT REMAINDED ON. AIRCRAFT RETURNED TO BLOCKS TRANSFERED TO DMI 9537 IAW MEL-24-24-CAT D.

Part: SWITCH — INOP (NR 1 ENGINE)

NR 1 ENGINE OIL PRESSURE LIGHT CAME ON IN FLIGHT, OIL PRESSURE AND QUANTITY OK, ENGINE SHUT DOWN AT 19:15 Z AS PER ARROW AIR ABNORMAL PROCEDURE, WINDMILLING PRESS, 17 PSI. REMOVED AND REPLACED NR 1 ENGINE OIL PRESS DIFF PRESS SWITCH, GROUND OPERATION CHECKED NORMAL IAW M/M 79-33-1 AND 71-00-00.

Part: ACTUATOR — NOT SECURED (SELECTOR VLV)

UNABLE TO PRESSURIZE CABIN ALTITUDE REACHED 10,000 A/C ALTITUDE WAS 10,000 NO DOOR WARNING LIGHTS ILLUMINATED. T/S FOUND REC FAN AIR SELECTOR VALVE ACTUATOR NOT SECURED. SECURED AIR SELECTOR VALVE ACTUATOR IAW M/M 21-21-5, OPS NORMAL ON RUN UP.

Part: RADIO ALT — INOPERATIVE (E/E COMPT)

CREW REMOVED AND REPLACED NR 2 RADIO ALT OFF FLAG IN/VIEW. REMOVED AND REPLACED NR 2 RADIO ALT, OPS NORMAL IAW 34-16-00.

Part: ACTUATOR — INOPERATIVE (HORIZ STAB)

CONTROL WHEEL SWITCHES ON CAPT AND FO FOR LONGITUDINAL TRIM INOP. ON PREFLIGHT SWAPPED TRIM ACTUATOR, REINSTALLED LOANER TRIM ACTUATOR, SYS OPS CHECK NORMAL IAW MM 27-43-0.

Part: ACTUATOR — DIRTY (SPOILER)

NO SPOILER DEPLOYMENT WITH REAR WHEELS SPIN UP. SPOILER HANDLE STIFF TO ACTUATE. FOUND BELL CRANK AND SPOILER HYD. ACTUATOR HAD EXCESSIVE BUILD-UP OF ANTI-CORROSION PAINT. REMOVED BUILD UP AND LUBE CRANK. SPOILER SYSTEM, OPS CHECKED GOOD IAW DC-8 M/M 27-60-0. AUTO SPOILERS OPS CHECKED GOOD IAW DC-8, M/M 27-60-2.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

BLOCK TURNBACK AFTER SPOOLED AND STABLE NR 1 OR NR 2 ENG COMPRESSOR STALL. FOUND PAPER IN INLET OF NR 2 ENGINE. REMOVED FOD (PAPER) FROM INLET, STARTED AND SPOOLED UP NR 2 ENGINE IAW DC-8 MM 80-00-0, NO DEFECTS NOTED AT THIS TIME.

Part: CONTROL CABLE — BROKEN (HORIZ STAB TRIM)

WHEEL LONGITUDINAL TRIM WILL NOT TRIM NOSE UP, SUITCASE HANDLE ARE SPLIT LEFT HANDLE FULL AFT. RIGHT HANDLE IN NEUTRAL POSITION. FOUND LONGITUDINAL TRIM CABLE 113A BROKEN. REMOVED AND REPLACED CABLE IAW DC-8 91-10-0 AND 91-10-2. INSTALLED CABLE PER MM 27-40-0, ADJUSTMENT, TENSION AND OPS. CHECK OK IAW 27-40-0. ASSY CABLE PER 20-11-0.

Part: SENSOR — MALFUNCTIONED (PAX DOOR)

MIA - FLT 627 - REJECTED T/O DUE MAIN CABIN DOOR LIGHT AND MASTER WARNING LIGHTS COMES ON INTERMITTENT. CHECK DOOR VISUAL AS NORMAL, OPEN AND CLOSE AGAIN LIGHTS GOES OUT. DEPART, ACCORDING AOM BRAKE COOLING CHART. CHECK MAIN CABIN DOOR OPEN AND CLOSE FEW TIMES WARNING LIGHT OK MM 52-10-0. (M)

Part: FUEL CELL — CORRODED (RT WING)

MIA - RIGHT WING FORWARD AUXILIARY TANK LOWER SURFACE HAS CORROSION. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED PER JOSSAIR CO E.O. 18R572001. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3, ITEM NR 31. (X)

Part: FUSE — BLOWN (NR 1/2 BUS)

LIGHTING BOLT STRUCK NEAR AIRCRAFT ON GROUND. GROUND POWER WENT OFF AIRCRAFT. AFTER ONE HOUR (STORM) POWERED AIRCRAFT. SMOKE CAME UP BETWEEN CABIN PRESS CONTROL PANEL. LEFT DC INOPERATIVE. SEVERAL AIRCRAFT SYSTEMS INOPERATIVE. ALL FOUR FIRE DETECTION INOPERATIVE. ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW MM 5-8-3, NO ABNORMALITIES NOTED. FOUND 100 AMPS FUSE TO NUMBER ONE AND TWO BUS OPEN. REPLACED FUSE IAW M/M 24-2-1, OPERATIONAL NORMAL. ALL SYSTEMS FUNCTIONING PROPERLY.

Part: STRIKER — LOOSE (PASS DOOR)

MIA - FLT 627 - AT 24,000 FEET LIGHT ON DOOR, (DOOR WARNING LIGHT ON) PERFORMED ACCORDING ABNORMAL CHECKLIST, DOES NOT CURE, RETURNED TO LICZ. T/S CHECKED MAIN GEAR DOOR UPLATCH RIGGING, FOUND LEFT DOOR STRICKER LOOSE, SECURED STRICKER, OPS CHECK NORMAL ON GROUND IAW 32-31-4. (M)

Part: TRIM ACTUATOR — ERRATIC (ELEVATOR)

AFTER ROTATION STAB SETTING WENT ALL THE WAY FWD. SAME AT ALL SPEEDS UP TO 320 KTS. RETURNED TO MIAMI WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED PTC ACTUATOR IAW MM 27-30-6. OPS CHECK NORMAL IAW MM 27-30-0 PILOT REPORTS ELEVETOR/STAB TRIM OPERATES NORMAL ON TEST FLIGHT.

Part: SKIN — DAMAGED (LT TE FLAP)

DURING D-CHECK, FOUND LEFT WING, INBOARD FLAP, LOWER SURFACE HAS A TEMPORARY REPAIR. REMOVED SECTION OF SKIN. FABRICATED AND INSTALLED NEW SECTION IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-1388. WORK ACCOMPLISHED UNDER ARROW FORM M3A, WORK ORDER 970101, ITEM NR 1388, CONTROL NR 1547.

Part: SPLICE — CORRODED (BS 660-680)

DURING D-CHECK, FOUND MIDSHIP ACCESSORY COMPARTMENT LONGERON 25 RIGHT SPLICE HAS CORROSION, FS 660 TO 680. REMOVED LONGERON SPLICE, CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101.2418. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2418, CONTROL NR 5921.

Part: CAP — MISDRILLED (LT WING)

DURING D-CHECK, FOUND LEFT WING AUX TANK UPPER T-CAP HAS SOME MISDRILLED HOLES. PLUGED MISDRILLED HOLES FABRICATED REPAIR STRAP AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2933. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2933, CONTROL NR 1941.

Part: FLOORBEAM — CORRODED (BS 1420)

DURING D-CHECK, FOUND AFT LOWER CARGO LEFT SIDE FS 1420, FLOORBEAM HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR ANGLE AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2436. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2436, CONTROL NR 5236.

Part: TRAP FITTING — CRACKED (RIGHT)

DURING D-CHECK, FOUND RIGHT HAND TRAPEZOID FITTING HAS FOUR CRACKS. REMOVED CRACKED TRAP, FITTING AND INSTALLED NEW TRAP FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5616481 AND SRM 51-1-20D, 51-3-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3067, CONTROL NR 5142A.

Part: SKIN — CORRODED (WS 329)

DURING D-CHECK, FOUND LEFT WING LEADING EDGE SKIN HAS CORROSION AT STATION XFS 329.00. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1285. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1286, CONTROL NR 1449.

Part: STRAP — CRACKED (NR 1 PYLON)

DURING D-CHECK, FOUND NR 1 ENGINE PYLON, UPPER SUPPORT STRAP HAS A CRACK. REMOVED SUPPORT STRAP. FABRICATED NEW STRAP AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DRAWING NR 5753033, 5753000 AND SRM 51-1-20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0581, CONTROL NR 8012.

Part: SPAR CAP — CORRODED (VERT STAB)

DURING D-CHECK, FOUND VERTICAL STABILIZER REAR SPAR CAP LEFT HAND HAS CORROSION. REMOVED SECTION OF SPAR CAP. MACHINED NEW SECTION OF SPAR CAP AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5611409 AND SRM 51-1-21. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0526, CONTROL NR 6019.

Part: SKIN — CRACKED (LT HORIZ STAB)

DURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS A CRACK ON SKIN. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0261, CONTROL NR 3015.

Part: SKIN — DAMAGED (LT HORIZ STAB)

DURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS TEMPORARY REPAIR. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER, 970101, ITEM NR 0268, CONTROL NR 3022.

Part: SKIN — CORRODED (WS 485-710)

DURING D-CHECK, FOUND LEFT HAND WING LEADING EDGE FROM STATION XFS 485 TO 710 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1378, CONTROL NR 1533.

Part: CUSP — CORRODED (BS 1140-1160)

DURING D-CHECK, FOUND RIGHT HAND CUSP AT FS 1140 TO 1160 HAS CORROSION. CUT OUT DAMAGED SECTION OF CUSP. FABRICATED AND INSTALLED NEW SECTION OF CUSP IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-5. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0106, CONTROL NR 5089.

Part: FRAME — CORRODED (BS 540)

DURING D-CHECK, FOUND FRAME AT FS 540 HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED NEW SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 799, CONTROL NR 5394.

Part: SKIN — CORRODED (WS 0-74)

DURING D-CHECK, FOUND RIGHT WING UPPER SURFACE SKIN HAS CORROSION FROM STATION XWO TO XRS 74. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1589, CONTROL NR 1562.

Part: SKIN — DAMAGED (LT WING)

DURING D-CHECK, FOUND LEFT WING NR 1 STUB LEADING EDGE HAS A TEMPORARY REPAIR. FABRICATED AND INSTALLED NEW DOUBLER IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98012105. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2833, CONTROL NR 1900.

Part: ACCESS PANEL — MISSING (RT MLG)

DURING D-CHECK, FOUND RIGHT HAND MAIN LANDING GEAR, KEEL BEAM INSPECTION ACCESS PANEL MISSING. FABRICATED AND INSTALLED NEW ACCESS PANEL IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW970101-3180. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3180, CONTROL NR 5172A.

Part: LONGERON — CORRODED (BS 1140-1170)

DURING D-CHECK, FOUND MAIN CABIN AT LONGERON 11 LEFT, WEB HAS CORROSION FROM FS 1140 TO 1170. FABRICATED STRAP AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW97010-2916. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2916, CONTROL NR 5095A.

Part: SKIN — CORRODED (VERT STAB)

DURING D-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE UPPER SECTION HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2856, CONTROL NR 6086.

Part: DOUBLER — DAMAGED (BS 74.125)

DURING D-CHECK, FOUND INSTALL TWO DOUBLERS AT FS 74.125 LEFT HAND FOR TEMPERATURE PROBES. FABRICATED AND INSTALLED TWO TEMPERATURE PROBES DOUBLERS IN ACCORDANCE WITH NEW SYSTEMS DRAWING 229-92-100 AND 229-921110. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3131, CONTROL NR 4497.

Part: CABLE GUIDE — BROKEN (WS 422)

DURING D-CHECK, FOUND LEFT WING FRONT SPAR AT STATION XFS 422.0 HAS A PHENOLIC CABLE GUIDE BROKEN. FABRICATED REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-0705. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0705, CONTROL NR 1214.

Part: FRAME — CRACKED (BS 1542)

DURING D-CHECK, FOUND MAIN CABIN FRAME IS CRACKED AT FS 1542. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED NEW FRAME SECTION AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3020. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 3020, CONTROL NR 5119A.

Part: SKIN — CORRODED (RT WING)

DURING D-CHECK, FOUND RIGHT WING NR 3 STUB LEADING EDGE UPPER SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2616. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2616, CONTROL NR 1886.

Part: FRAME — BENT (BS 300)

DURING D-CHECK, FOUND RIGHT HAND FS 300, RIB BENT, CUSP ANGLE AREA. CUT OUT DAMAGED SECTION OF FRAME. INSTALLED NEW SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0014, CONTROL NR 5009.

Part: SKIN — DENTED (BS 350)

DURING D-CHECK, FOUND MAIN CARGO DOOR CUTOUT, EXTERIOR SKIN AT FS 350, LOWER CORNER AREA HAS SEVERAL DENTS AND CORROSION. REMOVED CORROSION AND TRIMMED OUT AREA IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, ACTION NR 360499, FILE NR 98-02-010. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2508, CONTROL NR 5007A.

Part: BULKHEAD SKIN — CRACKED (BS 1400)

DURING D-CHECK, FOUND AFT LOWER CARGO COMPARTMENT FS 1400 BULKHEAD ACCESS PANEL IS CRACKED. REMOVED SKIN, FABRICATED NEW SKIN AND INSTALLED IN ACCORDANDE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98022303. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM 0324, CONTROL NR 5151.

Part: CUSP — CORRODED (BS 1200)

DURING D-CHECK, FOUND LEFT HAND CUSP AT FS 1200 HAS CORROSION. CUT OUT DAMAGED SECTION OF CUSP. FABRICATED AND INSTALLED NEW SECTION OF CUPS IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-5. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0160, CONTROL NR 5062.

Part: SKIN — CORRODED (LT WING)

DURING D-CHECK, FOUND LEFT WING OUTBOARD LEADING EDGE, INBOARD SECTION HAS CORROSION. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2497, CONTROL NR 1836.

Part: SKIN — CORRODED (LT TE FLAP)

DURING D-CHECK, FOUND LEFT WING, INBOARD FLAP SKIN HAS CORROSION. REMOVED SECTION OF SKIN. FABRICATED AND INSTALLED NEW SECTION OF SKIN IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-1525. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1525, CONTROL NR 1538.

Part: FRAME — CORRODED (BS 228)

DURING D-CHECK, FOUND ACCESSORY COMPARTMENT AT FS 228, CIRCUMFERENTIAL HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-0, 51-1-20D AND 51-3-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1690, CONTROL NR 4188.

Part: FRAME — CORRODED (CABIN)

DURING D-CHECK, FOUND MAIN CABIN AT RIGHT HAND CUSP, CIRCUMFERENTIAL HAS CORROSION. CUT DAMAGED SECTION OF FRAME. FABRICATED NEW SECTION OF FRAME AND REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-3 AND 51-1-20. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0100, CONTROL NR 5083.

Part: SUPPORT — CRACKED (RT WING)

DURING D-CHECK, FOUND RIGHT WING CENTER SECTION OF LEADING HAS A SUPPORT CRACKED. REMOVED CRACKED SUPPORT. FABRICATED NEW SUPPORT AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5770409 AND SRM 53-01-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1721, CONTROL NR 1689.

Part: FRAME — CRACK (BS 680)

DURING D-CHECK, FOUND MIDSHIP ACCESSORY COMPARTMENT, CIRCUMFERENTIAL FRAME HAS A 2 INCH CRACK AT STATION 680, BETWEEN LONGERON 35R AND 36. STOP DRILLED CRACK AND REMOVED DAMAGED EXISTING SPLICE. FABRICATED NEW SPLICE AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-3029. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3029, CONTROL NR 5123A.

Part: SKIN — CORRODED (LT WING)

DURING D-CHECK, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANDE WITH AVITAS ENGINEERING, EO 98AROW.021D-3007. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 3007, CONTROL NR 1953.

Part: SKIN — DAMAGED (BS 1400)

DURING D-CHECK, FOUND FUSELAGE EXTERIOR SKIN HAS A HOLE AT FS 1400. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1 AND 51-1-20D AND 51-1-2. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2952, CONTROL NR 5112A.

Part: FRAME — CORRODED (BS 640)

DURING D-CHECK, FOUND FRAME AT FS 640 AT CUSP AREA HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0132, CONTROL NR 5034.

Part: LONGERON — CORRODED (BS 680-710)

DURING D-CHECK, FOUND LONGERON 31 LEFT HAS CORROSION AT FS 680 TO 710. CUT OUT DAMAGED SECTION OF LONGERON. LOCATED DRILLED AND INSTALLED NEW SECTION OF LONGERON IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 51-1-20D AND 53-4-1 39A. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2996, CONTROL NR 5105A.

Part: SKIN — CORRODED (FUSELAGE)

DURING D-CHECK, FOUND FUSELAGE FORWARD TOPSIDE INSTALL DOUBLERS WHERE EXISTING OMEGA ANTENNAS WERE MOUNTED. FABRICATED FILLER AND DOUBLERS AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3136, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3136, CONTROL NR 5166A.

Part: SKIN — CORRODED (WS 423-525)

DURING D-CHECK, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN HAS CORROSION FROM STATION XFS 423 TO 525. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-3-2-, 51-1-21 AND 51-1-21D. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2939, CONTROL NR 5103A.

Part: SKIN — CORRODED (BS 1450)

DURING D-CHECK, FOUND FUSLAGE EXT SKIN FS 1450 HOOK TO LOCK REAR SERVICE DOOR HAS CORROSION. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED DOUBLER, FILLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.020D-0339. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0339, CONTROL NR 5188.

Part: DOUBLER — CORRODED (COCKPIT)

DURING D-CHECK, FOUND MAIN CABIN, COCKPIT FORWARD OF RUDDER PEDALS, FINGER DOUBLER HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.112D-2726. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2726, CONTROL NR 4406.

Part: SKIN — CORRODED (RT HORIZ STAB)

DURING D-CHECK, FOUND RIGHT HAND HORIZONTAL STABILIZER, INBOARD LEADING EDGE HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1 AND 51-1-20. WORK ACCOMPLISHED UNDER ARROW AIR JW3B, WORK ORDER 970101, ITEM NR 2464, CONTROL NR 3083.

Part: FRAME — CORRODED (BS 660)

DURING D-CHECK, FOUND MAIN CABIN FRAME AT STATION 660 HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED REPAIR SPLICES AND INSTALLED NEW SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 3094, CONTROL NR 5152A.

Part: SKIN — CORRODED (LT WING)

DURING D-CHECK, FOUND LEFT WING OUTBOARD LEADING EDGE LOWER SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2845. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2845, CONTROL NR 1902.

Part: LONGERON — CRACKED (FUSELAGE)

DURING D-CHECK, FOUND INSPECTED LEFT AND RIGHT HAND LONGERON 24 FOR CRACK GROWTH, FOUND CRACK UNDER RT MAIN BOLT. REPLACED LONGERON 24R HAND PER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2191, CONTROL NR 5809 AND RED BORDER NR 8064.

Part: FRAME — GOUGED (BS 400)

DURING D-CHECK, FOUND MAIN CABIN LONGERON NR 12 AT STATION 400 FRAME HAS GOUGE. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED FILLER AND REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2994. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2994, CONTROL NR 5113A.

Part: SKIN — CORRODED (WS 291)

DURING D-CHECK, FOUND LEFT WING UPPER LEADING EDGE SKIN HAS CORROSION AT STATION XFS 291.00. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOULBER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1285. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1285, CONTROL NR 1448.

Part: FILL PORT — CORRODED (FUSELAGE)

DURING D-CHECK, FOUND FUSELAGE EXT RIGHT FOWARD, WATER FILL PORT, CORROSION INSIDE. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0169, CONTROL NR 5025.

Part: LONGERON — CRACKED (FUSELAGE)

DURING D-CHECK, FOUND RIGHT HAND LONGERON 24 HAS A CRACK. REMOVED DAMAGED LONGERON. LOCATED, DRILLED AND INSTALLED NEW LONGERON 24 IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5753508 AND SRM 51-1-24, 51-1-20D AND 51-3-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2191, CONTROL NR 5809.

Part: FRAME — CORRODED (BS 1563)

DURING D-CHECK, FOUND MAIN CABIN, FRAME AT FS 1563 HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED NEW SECTION OF FRAME AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-0135. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0135, CONTROL NR 5037.

Part: FRAME — CORRODED (RT MLG WW)

DURING D-CHECK, FOUND RIGHT WHEEL WELL, FORWARD RIGHT LOWER CORNER FRAME HAS CORROSION AND IS CRACKED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3113. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 3113, CONTROL NR 5158A.

Part: FITTING — CORRODED (BS 1230)

DURINGD CHECK, FOUND LEFT HAND FS 1230 LONGERON 21 FLOORBEAM FITTING HAS CORROSION. REMOVED DAMAGED FITTING. FABRICATED AND INSTALLED NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING 9754064 AND SRM 51-1-20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2362, CONTROL NR 5814.

Part: FLOORBEAM — CORRODED (BS 255)

DURING D-CHECK, FOUND CABIN FLOORBEAM AT FS 255 HAS CORROSION. CUT OUT DAMAGED SECTION OF FLOORBEAM. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-2896. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2896, CONTROL NR 5090A.

Part: LONGERON — CORRODED (BS 680-720)

DURING D-CHECK, FOUND FUSELAGE CENTER SECTION, LONGERON 32L HAS CORROSION AT FS 680 TO 720. CUT OUT DAMAGED SECTION OF LONGERON. LOCATED, DRILLED, AND INSTALLED NEW SECTION OF LONGERON IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-0 AND 51-1-20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2947, CONTROL NR 5106A.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING D-CHECK, FOUND RIGHT HAND FWD SERVICE DOOR HAS DENT AND A CRACK. STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98030806. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2439, CONTROL NR 5976.

Part: FRAME — CRACKED (BS 1400)

DURING D-CHECK, FOUND MAIN CABIN RIGHT SIDE STATION 1400 FRAME IS CRACKED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED NEW SECTION OF FRAME AND REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1 AND 51-1-20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2928, CONTROL NR 5100A.

Part: FRAME — DENTED (BS 400)

DURING D-CHECK, FOUND MAIN CABIN RIGHT SIDE STATION 400 FRAME HAS A DENT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED REPAIR DOUBLER AND INSTALLED NEW SECTION OF FRAME IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2926. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2926 CONTROL NR 5099A.

Part: SUB FLOOR — CORRODED (BS 224)

DURING D-CHECK, FOUND ACCESSORY COMPARTMENT SUB FLOOR AT FS 224 HAS CORROSION. REMOVED SUB FLOOR. FABRICATED AND INSTALLED NEW SUB FLOOR IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-0007. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1650, CONTROL NR 4132.

Part: SKIN — PUNCTURED (FUSELAGE)

DURING D-CHECK, FOUND RIGHT SIDE FUSELAGE JUST FORWARD OF AFT PRESSURE BULKHEAD, BETWEEN LONGERON 26R AND 28R, SKIN IS PUNCTURED. CUT OUT DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3236, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3236, CONTROL NR 5180.

Part: SKIN — CORRODED (WS 710-885)

DURING D-CHECK, FOUND LEFT WING LEADING EDGE HAS CORROSION FORM STATION XFS 710 TO 885. REMOVED DAMAGED SECTION OF SKIN. FABRICATED DOUBLER, FILLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98ROW.021D-2372. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2372, CONTROL NR 5929.

Part: TRAP PANEL — CRACKED (LT MLG WW)

DURING D-CHECK, FOUND LEFT HAND WHEEL WELL, TRAPEZOID FITTING HAS A 7 INCH CRACK. REMOVED CRACKED TRAPEZOID, LOCATED, DRILLED AND INSTALLED NEW TRAPEZOID FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5616481 AND SRM 51-1-20D, 51-3-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1379, CONTROL NR 1534.

Part: KEEL BEAM — CORRODED (BS 680-720)

DURING D-CHECK, FOUND FUSELAGE CENTER SECTION KEEL BEAM FROM FS 680 TO 720 HAS CORROSION. CUT OUT DAMAGED SECTION OF KEEL BEAM. MACHINED NEW SECTION OF KEEL BEAM AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5613779 AND ACTION NR 358456, 358745, FILE NR 98-01-30-004/98-02-03-005. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2997, CONTROL NR 5107A.

Part: SKIN — CORRODED (WS 710-885)

DURING D-CHECK, FOUND LEFT WING LEADING EDGE EXTERNAL SURFACE HAS CORROSION FROM STATION 710 TO 885. CUT OUT DAMAGED SECTION. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1201. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1201, CONTROL NR 1422.

Part: FRAME — CRACKED (BS 1420)

DURING D-CHECK, FOUND MAIN CABIN LEFT SIDE STATION 1420 FRAME IS CRACKED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED NEW SECTION OF FRAME AND REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1 AND 51-1-20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3125, CONTROL NR 5159A.

Part: SKIN — CORRODED (LT WING)

DURING D-CHECK, FOUND LEFT WING INBOARD STUB LEADING EDGE SKIN UPPER SURFACE HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2855. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2855, CONTROL NR 1916.

Part: OVEN — REPLACED (GALLEY)

DURING D-CHECK, FOUND REMOVED OVEN AND INSTALLED MICROWAVE SYSTEM FOR COMPANY CONVINIENCE. REMOVED OVEN. FABRICATED MICROWAVE MOUNT AND INSTALLED MICROWAVE SYSTEM IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98032301. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3147, CONTROL NR 4500.

Part: ANGLE — CRACKED (LT WING)

DURING D-CHECK, FOUND LEFT WING FUEL DUMP SHROUD COVER ATTACH ANGLE IS CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY EO ARW.970101.3065. WORK ACCOMPLISHED UNDER ARROW AIR, INC FORM M3A, WORK ORDER 970101, ITEM NR 3065, CONTROL NR 1970.

Part: T-CAP — CORRODED (LT WING)

DURING D-CHECK, FOUND LEFT WING AUX TANK UPPER CAP HAS CORROSION AT ATTACHMENT HOLES. REMOVED DAMAGED T-CAP, AND INSTALLED NEW T-CAP FROM DOUGLAS AIRCRAFT COMPANY. INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 51-1-20 AND 51-1-21. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1209, CONTROL NR 1437.

Part: SKIN — CORRODED (VERT STAB)

DURING D-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE LOWER SECTION HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0542, CONTROL NR 6034.

Part: SKIN — CORRODED (WS 50)

DURING D-CHECK, FOUND RIGHT WING SURFACE AT STATION XRS 50 HAS CORROSION AND A CRACK. REMOVED CORROSION AND CUT OUT CRACKED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS, AND PARTS, EO 98012103. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2892, CONTROL NR 1926.

Part: SKIN — DAMAGED (LT HORIZ STAB)

DURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS TEMPORARY REPAIR. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0062, CONTROL NR 3014.

Part: BLOWOUT PANEL — MISSING (NR 3 ENGINE)

DURING D-CHECK, FOUND REMOVED FROM NR 3 ENGINE INBOARD COWLING BLOW OUT PANEL FOR AIRCRAFT 802. FABRICATED AND INSTALLED NEW BLOW OUT PANEL FOR NR 3 ENGINE IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.95141-0103, REV C, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER, 970101, ITEM NR 3152, CONTROL NR 7194.

Part: SKIN — DAMAGED (LT LE FLAP)

DURING D-CHECK, FOUND REMOVED TEMPORARY REPAIR LEFT WING LEADING EDGE SLOT AT STA XFS 526. PERFORMED REPAIR OF LEFT HAND WING LEADING EDGE SLOT AT XFS=526 AS APER EO 98012105 AND ARROW AIR RED BORDER NR 8071.

Part: SPAR CAP — CORRODED (VERT STAB)

DURING D-CHECK, FOUND VERTICAL STABILIZER, REAR SPAR CAP, LEFT AND RIGHT SIDE HAS CORROSION AT STATION 161. REMVOED CORROSION IN AREA. FABRICATED REPAIR DOUBLERS AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, ACTION NR 35887, FILE NR 98-01-005. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2514, CONTROL NR 3086.

Part: FRAME — CUT OUT (BS 1240)

DURING D-CHECK, FOUND CUT OUT CIRCUMFERENTIAL AT FS 1240 FOR REMOVAL OF CUSP SECTION. CUT FRAME SECTION. FABRICATED SPLICES AND INSTALLED FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2487, CONTROL NR 5988.

Part: STIFFENER — CUT (BS 980)

DURING D-CHECK, FOUND RIGHT HAND MAIN WHEEL WELL, CUT HORIZONTAL STIFFENER AT FS 980 TO FACILITATE LONGERON 24 REPLACEMENT. CUT STIFFENER AND FABRICATED REPAIR BLOCK AND ANGLES AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3043. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM 3043, CONTROL NR 5134A.

Part: SKIN — CORRODED (RT MLG DOOR)

DURING D-CHECK, FOUND RIGHT MAIN LANDING GEAR DOOR INTERIOR AREA HAS CORROSION. REMOVED DOOR SKIN. FABRICATED NEW SKIN AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 52-6-2 AND 51-3-2. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2406, CONTROL NR 5940.

Part: WEB — TORN (CABIN)

DURING D-CHECK, FOUND MAIN CABIN 9G BULKHEAD SUB FLOOR WEB IS TORN. REMOVED SUB FLOOR WEB. FABRICATED AND INSTALLED NEW SUB FLOOR WEB IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-007. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 980010, ITEM NR 007.

Part: BULKHEAD WEB — DAMAGED (BS 35)

DURING D-CHECK, FOUND FUSELAGE AT FS 35.0 BULKHEAD HAS TWO BIG HOLES AT CENTER SECTION. REMOVED BULKHEAD WEB. INSTALLED NEW SECTION OF WEB IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.980010-0031. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 980010, ITEM NR 0031, CONTROL NR 0031.

Part: FLOORBEAM — CORRODED (BS 1500)

DURING D-CHECK, FOUND MAIN CABIN FLOORBEAM AT FS 1500 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING EO 98AROW.021D-2478. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1478, CONTROL NR 5599.

Part: FLOORBEAM — CORRODED (BS 260)

DURING D-CHECK, FOUND MAIN CABIN FLOORBEAM AT FS 260 LEFT HAND HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-3128. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER, 970101, ITEM NR 3128, CONTROL NR 5162A.

Part: LONGERON — CORRODED (BS 857-879)

DURING D-CHECK, FOUND MAIN CABIN LONGERON NR 1 AT FS 857 TO 879 HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR BLOCK AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98012905. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0845, CONTROL NR 5433.

Part: FRAME — CORRODED (BS 1120)

DURING D-CHECK, FOUND FRAME AT FS 1120 AT CUSP AREA HAS CORROSION. CUT OUT DAMAGE SECTION OF FRAME. FABRICATED AND INSTALLED NEW SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0145, CONTROL NR 5047.

Part: DOOR — CORRODED (BS 158)

DURING D-CHECK, FOUND AFT LOWER FUSELAGE DOOR AT FS 1586 HAS CORROSION. CLEANED CORROSION FABRICATED DOULBER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-0198. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0198, CONTROL NR 5126.

Part: ACCESS DOOR — DAMAGED (BS 1586)

DURING D-CHECK, FOUND FUSELAGE LOWER ACCESS DOOR NR 60 AT FS 1586 IS DAMAGED. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW970101-0198. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0198, CONTROL NR 5126.

Part: FAIRING — DAMAGED (RT WING/FUS)

DURING D-CHECK, FOUND FUSELAGE RIGHT SIDE FORWARD OF WING, FAIRING SUPPORT HOLE IS ELONGATED. REAMED HOLE TO .375 DIAMETER AND FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS, AND PARTS, EO 98012104. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2914, CONTROL NR 5093A.

Part: SKIN — CORRODED (LT WING)

DURING D-CHECK, FOUND LEFT WING NR 1 STUB LEADING EDGE MATING SURFACE HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1522. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1522, CONTROL NR 1469.

Part: SKIN — CORRODED (LT WING)

DURING D-CHECK, FOUND LEFT WING OUTBOARD LEADING EDGE, INBOARD SECTION LOWER SKIN HAS CORROSION AND A CRACK. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2846 AND DOUGLAS AIRCRAFT COMPANY, SRM 51-1-21. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2846, CONTROL NR 1903.

Part: SKIN — CORRODED (RT WING)

DURING D-CHECK, FOUND RIGHT WING NR 4 STUB LEADING EDGE SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW-021D-1495. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1495, CONTROL NR 1496.

Part: RECEIVER — INOPERATIVE (NR 1 VOR/ILS)

DURING FINAL SEGMENT OF CLIMB, F/O'S RMI READS 180 DEGREE OPPOSITE FROM ALL OTHER INSTRUMENTS INCLUDING CAPTS HSI. REMOVED AND REPLACED NR 1 VOR/ILS RECEIVER, OPS CHECKED NORMAL IAW M/M 34-30-1.

Part: PROXIMITY SWITCH — OPEN (LT MLG)

ON APPROACH LEFT MAIN LANDING GEAR GREEN LIGHT NOT ON. DOORS NOT LATCHED AND GEAR NOT LATCHED LIGHT ON. AIRCRAFT LANDING WITHOUT INCIDENT. REMOVED AND REPLACED LEFT GEAR DOWN PROXIMITY SWITCH. PERFORMED GEAR RETRACTION TEST I/A/W M/M 32-30-0. NO DEFECTS NOTED. OPS CHECK NORMAL.

Part: VENT DOOR — OUT OF ADJUST (FUSELAGE)

UNABLE TO MAINTAIN CABIN PRESS AT FL 350. CABIN CLIMBED TO 14,000 FT WITH A DIFF PRESS OF 5 PSI. SUSPECT VENT DOOR OPENED IN FLT. DESCENDED TO FL 250 AND DIVERTED TO MROC WITHOUT FURTHER INCIDENT. FOUND NASI VENT DOOR OUT OF RIG. RERIGGED VENT DOOR IAW DACO M/M 52-36-1 OPS AND LEAK CHECKED ON THE GROUND.

Part: BALLAST — FAILED (COCKPIT)

AIRCRAFT DIVERTED TO SJU. WHILE IN CRUISE AT FL 330, 2150Z, SMOKE WAS NOTED COMING FROM F/O SIDE PANEL. EMERGENCY PROCEDURES WERE FOLLOWED AND AN OVERWEIGHT LANDING WAS MADE WITHOUT INCIDENT. TROUBLESHOOTING BY MTX LOCATED A BURNED OUT FLUORESCENT LIGHT BALLAST. BALLAST WAS REMOVED AND REPLACED, SYS OPS CHECKED NORMAL. OVERWEIGHT LANDING INSPECTION REVEALED NO STRUCTURAL DAMAGE.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT DOES NOT DISARM. DOME LIGHT STAYS ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED OK IAW MM 3-50-00.

Part: OIL SYSTEM — FAILED (NR 3 ENGINE)

AIR TURNBACK AFTER APPROXIMATELY 15 MINUTES IN FLIGHT FROM JFK TO SDQ. SHUTDOWN NR 3 ENGINE DUE TO LOSS OF OIL QUANTITY. AIRCRAFT RETURNED TO JFK WHERE MAINTENANCE REPORTED INTERNAL FAILURE OF THE ENGINE OIL SYSTEM. THREE-ENGINE FERRIED AIRCRAFT TO MIAMI FOR ENGINE CHANGE. (M)

Part: SKIN — CRACKED (WS 315 LE)

DURING C-CHECK, FOUND R/W UPPER SURFACE LEADING EDGE CRACKED AT XFS 315. CUT OUT DAMAGED AREA FABRICATED 7075-T6 .063 FILLER AND 7075T6-071 DOUBLER AND INSTALLED IAW SRM 57-2-1. (M)

Part: SKIN — CORRODED (RT HORIZ STAB)

DURING C-CHECK INSPECTION, FOUND RT HORIZONTAL STABILIZER UPPER TIP WITH EXFOLIATION (LEVEL 2) CORROSION. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-1. SEALED REPAIR IAW SRM 51-20-0. (X)

Part: FLOOR WEB — CRACKED (CARGO COMPT)

DURING C-CHECK, FOUND 'A' PIT FLOOR WEB CRACKED. STOP DRILLED SMALL CRACK IAW WITH SRM 53-2-0. ARROW AIR WORKORDER NR 950007-5153 (0396). (M)

Part: BLKHD BEAM — CRACKED (FS 1606)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD AFT SIDE THIRD HORIZONTAL BEAM FROM BOTTOM CRACKED AT BL ZERO. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-20D AND 53-20-0. ARROW AIR WORK ORDER NR 950007-6006 (0106). (M)

Part: CIRCUMFERENTIAL — CRACKED (FS 410)

DUIRNG C-CHECK, FOUND MAIN CABIN CIRCUMFERENTIAL CRACKED AT FS 410 BETWEEN L7R AND L8R. CUT OUT DAMAGED AREA, AND FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0. ARROW AIR WORK ORDER NR 950007-5146 (0378). (M)

Part: FLOOR SUPPORT — CRACKED (AFT LWR CARGO)

AFT LOWER CARGO COMPARTMENT, FS 1100 AND STR 32L AND STR 35L. FRAME ATTACH FLOOR SUPPORT IS CRACKED AT 2 PLACES. W.O. 95007, CTL NR 5161, NR 0412. REMOVED FLOOR SUPPORT, WELDED CRACKS PER D.P.S. 10225 AND REINSTALLED FLOOR SUPPORT IAW SRM 51-1-20D AND SRM 51-1-21.

Part: SIDE BRACE — CORRODED (LT MLG)

DURING C-CHECK INSPECTION, FOUND LEFT MLG SIDE BRACE LUGS ON STRUT WITH INTERNAL PITTING. CLEANED LUGS, FABRICATED BUSHINGS IAW OHM 32-1-1B. INSTALLED SIDE BRACE BUSINGS IAW OHM 13-1-6. REINSTALLED SIDE BRACE ASSEMBLY IAW MM 32-11-5. (M)

Part: CRANK — CORRODED (RUDDER)

DURING C-CHECK INSPECTION, FOUND RUDDER TAB CONTROL CRANK WITH LEVEL 2 CORROSION. CORROSION REMOVED. REPLACED RUDDER CONTROL CRANK IAW MM 27-21-2. RIGGED TAB PER MM 27-13-3. OPS CHECK NORMAL. (M)

Part: SKIN — CRACKED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD LEADING END HAS (CORNER) PANEL CHAFFING AND CRACKED. REMOVED PANEL AND FABRICATED REPLACEMENT IAW SRM 53-1-0. INSTALLED PANEL SRM 53-1-0 AND 51-1-20. (M)

Part: BUSHING — PITTED (LT MLG)

DURING C-CHECK INSPECTION, FOUND LEFT MLG SIDE BRACE LUGS ON STRUT HAD INTERNAL PITTING. REMOVED SIDE BRACE AND ROUTED TO SHOP FOR OVERHAUL. RE-BRUSHED STRUT PER MM 32-1-8, PAGE 402E. REINSTALLED SERVICEABLE SIDE BRACE PER MM 32-11-3. OPS NORMAL IAW MM 32-00-00. (X)

Part: SKIN — CRACK (WS 240 LE)

DURING C-CHECK, FOUND LT LOWER WING L/E LOOSE, FASTENERS AT APPROXIMATELY XFS 240.000; FOUND SMALL CRACK AT FASTENER HOLE. THE DAMAGED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED TO RESTORE THE LOST STRENGTH PER E.O. NR 9502274 AND SRM 51-1-8. (X)

Part: BRACKET — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND NR 1 PYLON LEFT SIDE CENTER COWL SUPPORT FITTING SUPPORT BRACKETS ARE CRACKED. REMOVED AND REPLACED SUPPORT BRACKETS AS PER SRM 54-2-1. (M)

Part: SUPPORT — CRACKED (FS 1120)

DURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT FS 1120 L35-32L FRAME ATTACH FLOOR SUPPORT CRACKED AT TWO PLACES. REMOVED FLOOR SUPPORT, WELDED CRACKS PER DPS 102.25 AND REINSTALLED FLOOR SUPPORT IAW SRM 51-1-20D AND 51-1-21. ARROW AIR WORK ORDER NR 950007-5162 (0409). (M)

Part: PANEL — CORROSION (VERT STAB)

DURING C-CHECK, FOUND VERTICAL STABILIZER TOP LEADING EDGE LEFT SIDE LEVEL 2 CORROSION. REMOVED CORROSION, FOUND BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-1 FIG 4. (M)

Part: CARGO TRACK — CORRODED (AFT LWR CARGO)

AFT LOWER CARGO COMPARTMENT, LT TRACK, HAS LEVEL II CORROSION AT FS 1080 - FS 1120, W.O. NR 950007, C/N 5163. REMOVED DAMAGED AREAS, TREATED, PRIMED AND INSTALLED NEW SECTION OF TRACKS PER SRM 53-2-3, AND SRM 51-1-21D.

Part: ANGLE — CRACKED (MAIN CARGO DOOR)

DURING C-CHECK, FOUND MAIN CARGO DOOR LATCH SUPPORT ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-1-21, 51-3-0 AND 53-2-0. (M)

Part: L/E SKIN — CRACKED (RT WING)

DURING C-CHECK, FOUND RIGHT WING LEADING EDGE BETWEEN NR 3 AND NR 4 ENGINES AT APPROXIMATE MID SECTION LOWER RIB SUPPORT PLATE WITH 2 CRACKS EMINATING FROM FASTENER HOLES. REMOVED AND FABRICATED REPLACEMENT PANEL PREPPED AND INSTALLED IAW SRM 57-2-1 PG 155/156 AND 51-1-8. (M)

Part: INTERCOSTAL — CORRODED (FS 220)

DURING C-CHECK, FOUND FORWARD ACCESS COMP VERT STIFFENER AT L-28L AND FS 208.00 HAS LEVEL 2 CORROSION. CUT OFF CORROSION SECTION OF STIFFENER, FABRICATED NEW SECTION OF STIFFENER FROM .071 7075-T6 AS PER SRM 53-1-0 AND SRM 52-2-0. (M)

Part: WEB — CRACKED (FS 35)

DURING C-CHECK, FOUND FORWARD FUSELAGE STRUCTURE JUST BELOW RADOME SUPPORT RODS, CRACKED LEFT AND RIGHT SIDE. ROUTED OUT CRACKED MATERIAL BLENDED, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0. (M)

Part: PANEL — CORRODED (RT SLOT)

RIGHT WING OUTBOARD SLOT MIDDLE PANEL HAS LEVEL 2 CORROSION, REF CPCP 027 115R 0551. FOUND AREA BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER IAW EO 9503061. (X)

Part: SLOT DOOR — CORRODED (RT TE FLAP)

DURING C-CHECK INSPECTION, FOUND RT WING OUTBOARD SLOT DOOR WITH LEVEL 2 CORROSION AT L/E, REF CPCP 031 116R0551. FABRICATED DOUBLER USING STAINLESS STEEL .040 301 1/2 HARD IAW EO NR 9503061 AND SRM 51-1-8. (X)

Part: SLOT DOOR — CORRODED (LE FLAP)

RT WING OUTBOARD SLOT DOOR HAS CORROSION LEVEL II AT L/E. REF N/R 1117 WO 950015.

Part: FITTING — BROKEN (DOOR FRAME)

DURING C-CHECK, FOUND 'B' BELLY LOWER DOOR FRAME SECOND FROM ATT 'T' BOLT BRACKET BROKEN IN HALF. REMOVED FITTINGS, FOUND AREA CORRODED REMOVED CORROSION AND TREATED AND PRIMED IAW SRM 51-1-8. REINSTALLED FITTING IAW SRM 51-3-0. RESEALED AREA WITH PRC 1422 B1/2 IAW SRM 51-1-16. (M)

Part: SUPPORT — CRACKED (FS 600)

DURING C-CHECK, FOUND FLOOR SUPPORT CRACKED AT FS 600 BETWEEN L35L AND L36L. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-20-0. ARROW AIR WORK ORDER NR 950007-5164 (0411). (M)

Part: SKIN — CORRODED (WS 304-416)

L/E BETWEEN NR 3 AND 4 ENGINE HAS CORROSION LEVEL II AND DELAMINATION OF FASTENER HOLES (UPPER) XFS 304 TO XFS 416. REF N/R 1102 W/O NR 950007.

Part: SKIN — CORROSION (WS 69.5 LE)

LEFT WING LEADING EDGE WS 69.500 AT FRONT SPAR, SMALL AREA AROUND SCREW, HAS CORROSION LEVEL II UPPER SURFACE. REMOVED CORROSION, FOUND AREA BEYOND LIMITS, FABRICATED DOUBLER AND FILLED REWORKED AREA IAW SRM 57-24. COMPLETED THICKNESS CHECK, TREATED, PRIMED, AND INSTALLED IAW SRM 57-2-1, F837.

Part: SUPPORT PLATE — CRACKED (WS 341.5)

L/E BETWEEN NR 3 AND 4 ENGINE AT XFS341.500 RIB LOWER SUPPORT PLATE HAS TWO CRACKS EMANATING FROM FASTENER HOLES. REF N/R 1101 WO NR 950007.

Part: SKIN — CORROSION (FS 857)

CORROSION AT FS 857.0, LEFT, IN THE WING BOX AREA. PERFORMED REPAIRS PER E.O. 9502201, W/O 950040, ITEM 9026.

Part: INTERCOSTAL — CRACK (FS 1600.0)

FS 1600, STR 28L, INTERCOSTAL IS CRACKED. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW INTERCOSTAL PER ORIGINAL HEAT TREATED TO 7075-T6 AND INSTALLED PER SRM 53-1-0. DOCUMENTED UNDER W/O 950007, ITEM 5110.

Part: SKIN — CORRODED (WS STA XFS 885)

EXFOLIATING CORROSION AROUND PREVIOUS REPAIRS ON LEFT WING LEADING EDGE UPPER SURFACE, WS XFS 885, WS XFS 890, XFS 908, AND XFS 920. REMOVED SECTION OF THE LEADING EDGE, REMOVED CORROSION, FOUND BEYOND LIMITS. ACCOMPLISHED REPAIR PER SRM 57-2-1, SRM 51-1-6, AND SRM 51-1-8.

Part: INTERCOSTAL — CRACKED (FS 1600)

DURING C-CHECK, FOUND MAIN CARGO COMPARTMENT AFT BULKHEAD FS 1600 AT L28L HAD CRACKED INTERCOSTAL. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-1-8, 51-1-20 AND 53-1-0. ARROW AIR WORK ORDER NR 950007-5110 (0249). (M)

Part: SKIN — CORRODED (ELEVATOR)

DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION BEYOND LIMITS ON ELEVATOR STA XE 176.156. REMOVED DAMAGED SKIN. FABRICATED AND INSTALLED NEW SKIN IAW DER DRAWING ARW.950007-0169. REBALANCED ELEVATOR IAW SRM 51-4-0. (X)

Part: SPAR — CORRODED (FS 857)

CENTER TANK (WING) TOP AFT SPAR FLANGE (CAP) HAS LEVEL II CORROSION ON TOP OF HORIZONTAL FLANGE AROUND FASTENER HEADS AT BL 23L FS 857 REF N/R NR 5086.

Part: STRESS PLANK — DAMAGED (NR 4 PYLON)

DURING INCIDENT, INSPECTION FOUND NR 4 PYLON INBAORD STRESS PANEL (STATIONARY PLANK) BENT. REMOVED AND REPLACED NR 4 PYLON INBOARD STATIONARY STRESS PLANK PER DAC DRAWINGS NR 5753010 AND 5753000. (M)

Part: RIB — BENT (WS 761.695)

DURING INCIDENT INSPECTION, FOUND RIGHT WING RIB SUPPORT FOR WING TIP AT STA XW 761.695 DAMAGED AT LEADING EDGE AREA. FABRICATED NOSE SECTION OF BULKHEAD FROM .071 INCH 7075-0, AND NOSE DOUBLER AND SPLICE DOUBLER FROM .080 INCH 7075-0. HEAT TREATED, PRIMED, AND INSTALLED ON WING IAW DER EO ARW.950031-0036.

Part: SKIN — DAMAGED (WS 763-636)

DURING C-CHECK INSPECTION, FOUND RT WING OUTBOARD TRAILING EDGE UPPER SURFACE PANEL DAMAGED FROM STA XW 763.0 TO XW 636.0. REPAIRED PANEL IAW SRM 51-1-9 AND DER EO 950031-0024. (X)