N366FE

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 82,548 hrs · 34,724 cycles

DURING EMERGENCY LIGHT TEST, RECEIVED LEVEL 1 ALERT; EMERGENCY LIGHT BATTERY ONE LOW. R & R EMERGENCY LIGHTS POWER SUPPLY. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 82,326 hrs · 34,585 cycles

APPEARS TO BE A CRACK IN RADIUS ON LT INBD FUELING PNL. PERFORMED HFEC INSP ON NEW CUT OUT IAW NTM PT 6, NO CRACK INDICATION FOUND. FABRICATED REPAIR DOUBLER & FILLERS FROM PREVIOUSLY VERIFIED MATERIAL IAW SRM 57-10-00. MX REQUEST OK TO INSTALL REPAIR PARTS. INSTALLED REPAIR DOUBLER & FILLERS AT NOTED LOCATION IAW SRM 57-10-00 FIG 68 & EA 8-5730-T0308584 PT1. LT WING LE SKIN CRACK AT INBD CORNER OF FUELING PANEL AT XOS=605-612. INSTALLATION COMPLETE SUBJECT TO FINAL APPROVAL & SURFACE RESTORATION. COMPLIED WITH PART 1 OF EA 8-5730-T0308584.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 81,544 hrs · 34,182 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR UPPER ANGLE VERTICAL TANG HAS TWO CRACKS AT THE UPPER ROW OF FASTENERS COMING OUT FROM UNDER WASHER , SECOND AND THIRD FASTENER HOLES. CRACKS ARE BEYOND BLEND LIMITS. REAMED HOLES TO REMOVE CRACK INDICATIONS. PLUGGED AND REAMED TO FASTENER DIMENSION INSTALLED DOUBLERS IAW EA 8-5510-T0303138.

Part: SUPPORT FITTING — CRACKED (MAIN CARGO) · airframe 81,544 hrs · 34,182 cycles

MCD LOWER FRAME 6 SUPPORT FITTING IS CRACKED AT "C" HOLE. VERIFIED WITH HFEC AND BORESCOPE. R & R NR 6 SUPPORT FITTING MCD SPOOL REF SRM 51-31-01, VOL II.

Part: SILL — CORRODED (ZONE 100) · airframe 81,544 hrs · 34,182 cycles

AFT LOWER CARGO COMPARTMENT DOOR SILL LOWER WEB AT BS 1835, JUST AFT OF AFT LATCH SPOOL FITTING, DOOR SILL WEB IS CORRODED. REMOVED CORROSION IAW SRM 53-50-00. REPAIRED IAW EA 8-5316-T03085A.

Part: SWITCH — FAILED (ESCAPE SLIDE) · airframe 80,690 hrs · 33,736 cycles

R1 EVACUATION SLIDE PRESSURE PRESS TO TEST INDICATING INOPERATIVE. R & R R1 DOOR ESCAPE SLIDE PRESSURE PRESS-TO-TEST SWITCH IAW MM 25-61-03-2, OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: BULKHEAD WEB — CRACKED (BS 1521) · airframe 80,466 hrs · 33,605 cycles

RIGHT BULKHEAD CRACKED 25 INCHES FWD OF BS 1521 AND 19 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED BULKHEAD IAW SRM 53-00 -01, FIG 10.

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 78,971 hrs · 32,793 cycles

RIGHT WING TE FLAP UPPER SKIN CORRODED OUT OF LIMITS. REPAIRED SKIN IAW SRM 57-10-00, FIG 86.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 78,971 hrs · 32,793 cycles

LEFT INBD FLAP UPPER SURFACE, DENTED 86" FROM INBD AND 6.5" FROM T/E. FOUND OUT OF LIMITS IAW SRM 51-80-01, PG 1, PARA 2. REPAIRED SKIN IAW SRM 57-00-01, FIG 4. (MAJOR)

Part: CABLE — OUT OF LIMITS (R1 DOOR) · airframe 78,971 hrs · 32,793 cycles

R1 DOOR SEQUENCE CABLE FOR AIR BOTTLE IS BINDING FOUND CABLE ADJUSTMENT OUT OF LIMITS. CABLE MOVEMENT GOOD. ADJUSTED AIR BOTTLE CABLE IAW MM 52-11-00-5. OPS CHECKED GOOD IAW MM 52-11-00-5 STEP 3G.

Part: CABLE — BINDING (R1 DOOR) · airframe 78,971 hrs · 32,793 cycles

R1 DOOR SEQUENCE CABLE FOR UPLOCK IS BINDING REMOVED AND REPLACED UPLOCK/CLOSE CABLE IAW AMM 52-11-12-2. ADJUSTED IAW AMM 52-11-00-5. OPS CHECKED GOOD.

Part: MOTOR — BINDING (R1 DOOR) · airframe 78,971 hrs · 32,793 cycles

R1 DOOR SEQUENCE CABLE FOR DECLUTCH IS BINDING. REMOVED AND REPLACED AC MOTOR AND ADJUSTED DECLUTCH CABLE IAW MM 52-11-01-2 AND 52-11-00-5. OPS CHECKED GOOD IAW MM 52-11-00-5 STEP 3G.

Part: ROLLER — GOUGED (LT INBD FLAPWELL) · airframe 78,971 hrs · 32,793 cycles

LEFT INBOARD FLAP WELL LOWER FORWARD ROLLER FITTING ASSY GOUGED. R & R LEFT INBOARD LOWER DUAL BRACKET ASSY IAW SRM 51-31-01.

Part: SEAT TRACK — WORN (BS 1251) · airframe 78,971 hrs · 32,793 cycles

SEAT TRACK, FS 1251 LBL 75, HAS WORN LOBE. CHECKED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG. 5. R & R SEAT TRACK IAW SRM 53-70-00 FIG 1 SH 2.

Part: SEAT TRACK — WORN (BS 1320) · airframe 78,971 hrs · 32,793 cycles

SEAT TRACK FS 1320 RBL 28 HAS WORN LOBE. FOUND OUT OF LIMITS IAW SRM 53-70-00 FIG 5. CUT OUT DAMAGED PART REPAIRED IAW SRM 53-70-00 FIG 1 AND SRM 51-31-01. MAJOR REPAIR.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 78,644 hrs · 32,609 cycles

DURING PREFLIGHT FOUND EMERGENCY LIGHT TEST SHOWS "EMER LT BATT 1 FAIL". R & R EMERGENCY LIGHTING BATTERY IAW AMM 33-51-01-4, OK FOR SERVICE.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 78,644 hrs · 32,609 cycles

DURING PREFLIGHT CHECK FOUND L1 DOOR EMERGENCY LIGHT LENS DAMAGED ON FLOOR. RELEASED FOR SERVICE IAW MEL: 33-50-02. REPLACED L1 DOOR EMERGENCY LIGHT LENS COVER IAW SMP.

Part: LENS — DAMAGED (EMERGENCY LIGHTS) · airframe 78,644 hrs · 32,609 cycles

DURING PREFLIGHT CHECK FOUND L1 DOOR EMERGENCY LIGHT LENS DAMAGED ON FLOOR. RELEASED FOR SERVICE IAW MEL: 33-50-02.

Part: SWITCH — FAILED (FIRE AGENT) · airframe 78,312 hrs · 32,442 cycles

FOUND NR 2 ENGINE FIRE AGENT 1 LOW LIGHT ILLUMINATED WHILE PREFORMING ENGINE RUN CHECK LIST FOR REQUAL. TROUBLESHOT PROBLEM TO A BAD AGENT 1 LOW SWITCH, L2-216, AT THE APU GROUND CONTROL PANEL. R & R L2-216 AND L2-217 NR 1 AND NR 2 AGENT LOW LIGHTS AT REMOTE APU CONTROL PANEL IAW CHAP 20 SMP. RECONNECTED WIRE E102-89-02 AT LIGHT L2-216 TERMINAL 2. CHECKED AGENT LOW LIGHTS IN COCKPIT ALL LIGHTS OUT. INSTALLED NR 2 AGENT LOW LIGHT CAP AS NEEDED FOR SERVICE IAW SMP'S. ACFT OK FOR SERVICE.

Part: ENGINE — VIBRATION (NR 1) · airframe 78,241 hrs · 32,401 cycles

SHUTDOWN ENG NR 1 INFLIGHT FOR UNUSUAL VIBRATIONS. VIBES START AT 91 PERCENT - AND VERY NOTICABLE ABOVE 94 PERCENT - LIGHT TO MEDIUM "SHUDDER" RAPTED VIBRATION. REMOVED NR 1 ENGINE SPINNER ASSY & FIRST STAGE FAN ROTOR BLADES IAW MM 72-21-00-4. LUBED IAW AMM 72-21-00-4. INSPECTED MASTER CHIP DETECTOR. NO METAL FOUND ON DETECTOR. INSTALLED NR 1 ENG FAN BLADES & SPINNER. IAW MM 72-21-00-4. PERFORMED VSV RIG CHECK ON NR 1 ENGINE REF AMM 73-20-01-2-0; FOUND IN RIG. PERFORMED VIBRATION SURVEY ON NR 1 ENG REF AMM 72-00-00-5; WITHIN LIMITS. NO VIBRATION ON VIBE EQUIPMENT OR FELT DURING MULTIPLE RUNS AT TAKEOFF POWER.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,787 hrs · 32,165 cycles

DURING THE EMERGENCY LIGHT TEST RECEIVED EMERG BAT 1 LOW ALERT. R & R NR1 EMERGENCY LIGHT BATTERY REF33-51-01-4-0. OPS CHECKED GOOD ACFT OK TO CONTINUE.

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 76,574 hrs · 31,549 cycles

ON FIRST LANDING ATTEMPT, GOT 3 RED ON PANEL AND CONFIG PAGE (TRIED PUSHING DOWN ON HANDLE, NO HELP). RAN CHECKLIST AND PUT GEAR HANDLE DOWN THE SECOND TIME WITH FORCE, GOT 3 DOWN GREEN ON ALL INDICATIONS. HANDLE ASSY INSTALLATION REPLACED. ADJUSTED LANDING GEAR CONTROL MECHANISM AS REQUIRED. REF MM 32-31-01-5. JACKED ACFT AND SWUNG GEAR SEVERAL TIMES REF AMM 32-30-00-5 EXTENSION AND RETRACTION. SYS POS CHECKS NORMAL.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 76,264 hrs · 31,398 cycles

ABORT TAKEOFF, 75 KNOTS, ENG 3 EXCEEDANCE ON N2 PEAK 101, .2 RED: 101.0 FOR 2.3 SECONDS NO RESTRICTION, REF: AMM 72-00-00-6, NR 3 ENGINE N2 EXCEEDANCE 101.2 WILL REQUIRE CORE COMPRESSOR AND HPT BORESCOPE WITH IN 10 CYCLES INSPECTED EXHAUST NOZZLES FOR PARTICLES IAW MM 72-0 0-00-6. NO PARTICLES FOUND. PERFORMED BORESCOPE FOR EXCEEDANCE, NO DISCREPANCIES NOTED. TERMINATING ACTION ACCOMPLISHED FOR AMM 72-00-00-6 AT 76,273:34 H31, 404 C. REINSTALLED CORE COMPRESSOR AND HPT BORESCOPE PLUGS REF AMM 72-00-00-6.

Part: SKIN — CORRODED (BS 1681-1701) · corrosion level 3 · airframe 75,229 hrs · 30,913 cycles

LOWER FUSELAGE DISHED RIVET AT LONG 441 STATION 1682. REPAIRED FUSELAGE SKIN IAW DC 10 SRM 53-20-00 FIG 6.

Part: SKIN — CORRODED (BS 1761-1771) · airframe 75,229 hrs · 30,913 cycles

LOWER FUSELAGE DISHED RIVET AT LONG 48L STA 1761. REPAIRED AREA REF SRM 53-20-00.

Part: SKIN — CORRODED (BS 1741-1751) · corrosion level 3 · airframe 75,229 hrs · 30,913 cycles

LOWER FUSELAGE DISHED RIVET AT LONG. 46L STA 1741. REPAIRED AREA REF SRM 53-20-00.

Part: LINK — DAMAGED (RT MLG) · airframe 75,137 hrs · 30,868 cycles

RIGHT MAIN GEAR INDICATED UNSAFE ON DEPARTURE COMPLIED WITH QRH AND DIVERTED TO LAX. FOUND RT CRANK ASSY UPPER BOLT NUT MISSING. LINK ASSY FOUND DAMAGED REMOVED AND REPLACED LINK ASSEMBLY AND PERFORMED OPS CHECK IN REF TO MM 32-61-15-4. CHECKS GOOD OK TO CONTINUE.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 74,564 hrs · 30,600 cycles

35 MINUTES INTO FLT ENG NR 2 OIL QTY DROPPED TO ZERO. TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASING TO APPROX (15 PSI) FLUCTUATING /- 5 PSI WHEN ENGINE WAS SHUT DOWN IN ACCORDANCE W/QRH. WINDMILLING PRESSURE GREATER THAN 2 PSI.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 74,564 hrs · 30,600 cycles

35 MINUTES INTO FLT, ENG NR 2 OIL QTY DROPPED TO ZERO, TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASING TO APPROX (15 PSI) FLUCTUATING /- 5 PSI WHEN ENGINE WAS SHUT DOWN IN ACCORDANCE W/QRH. WINDMILLING PRESSURE GREATER THAN 2 PSI. REPLACED NR 2 ENGINE UPPER HYDRAULIC PUMP.

Part: NONE — NONE · airframe 74,118 hrs · 30,391 cycles

REJECTED TAKEOFF FOR WINDSHEAR AURAL ALERT 80 KTS,34 DEG C ,386K FACT 05 JUN08 21:47 AFW U CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 73,396 hrs · 30,049 cycles

DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON EXTERNAL SKIN AT FWD CARGO DOOR AFT JAMB WAS FOUND DAMAGED. REPAIR AS BEEN REPLACED WITH A NEW ONE IAW SRM 53-50-00 FIG 9.

Part: SKIN — MISREPAIRED (LT WING) · airframe 73,396 hrs · 30,049 cycles

DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON LT DROOPED L/E SKIN WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 57-10-00, FIG 55, VOL I.

Part: FRAME — MISREPAIRED (FUSELAGE) · corrosion level 2 · airframe 73,396 hrs · 30,049 cycles

DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 859 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 73,396 hrs · 30,049 cycles

DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 824 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 73,396 hrs · 30,049 cycles

DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 879 BETWEEN LONG NR 47R AND 47L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-30-00, FIG 5, VOL I.

Part: FRAME — MISREPAIRED (FUSELAGE) · corrosion level 2 · airframe 73,396 hrs · 30,049 cycles

DURING REPAIR ASSESSMENT PROGRAM AN EXISTING REPAIR ON FRAME CAP AT STA 840 BETWEEN LONG NR 50R AND 50L WAS FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REPAIR HAS BEEN REPLACED WITH A NEW ONE IAW SRM 53-30-00, FIG 5, VOL I.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), LT WING T/E ON UPPER SKIN OUTBOARD FLAP XOF 620 FOUND DENT 1" BY 1" AND A TEE ANGLE WITH CRACK 1 INCH LONG REPLACED PANEL ARC 1959U27 FOR SRM 51-35-01 VOL II.

Part: FITTING — CRACKED (100) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE BAY JAMB STRUCTURE FRAME TO STA 528 DEFORMED CORROSION AND CRACK LONG 2" ON SUPPORT FITTING. REPLACED FRAME ACA3347-3 AND FITTING ACA3799-501 FOR SRM 51-35-01 VOL II.

Part: DOOR FRAME — DEFORMED (FUSELAGE) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION COMPT LT SIDE BAY JAMB STRUCTURE FRAME AT STA 486 DEFORMED REPAIRED FOR SRM 53-30-00 FIG 5 VOL I.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING THE HOLES OF THE BOLTS WITH CORROSION. PERFORMED CORROSION REWORK REAMED HOLES, PERFORMED INSPECT HFEC AND INSTALLED BUSHINGS FOR SRM 53-50-00 FIG 17.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) FOUND IN LOWER FWD CARGO LIGHT CORROSION ON CHANNEL FROM STA 759 TO STA 879 X= 59. REMOVED CORROSION FOR SRM 51-21-01 VOL 2. PERFORMED CHECK LIMIT THICKNESS IS OUT LIMITS. REPLACED CHANNEL FOR SRM 53-70-00 FIG 7 VOL I.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), AVIONIC COMPT AT STA 449 RT AND X= -10 FRAME WITH HOLE OVALIZED PERFORMED REPAIR FOR SRM 53-30-00 FIG 4 VOL I.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), CTR SECTION BOX WHEEL WELL AREA STA 1370 LT SIDE XCW 31.500 KEEL FITTING APB7078-1 WITH CRACK 5" LONG REPLACED KEEL FITTING FOR SRM 51-33-01 AND SRM 51-32-01.

Part: FRAME — CRACKED (NR 3 PYLON) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK) PYLON NR 3 FOUND INTERNAL SIDE FRAME BROKEN AND DEFORMED. REPLACED STRAP P/N AVB7123-3, ANGLE P/N AUB7123-5, ZEE P/N AUB7123-7, CLIP P/N AUB7124-2 FOR SRM 51-33-01 VOL II.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE FROM STA 561 TO STA 587 STRINGER 48 WITH CRACK AND SEVERAL CORROSION REPAIRED WITH REFERENCE SRM 53-10-00 FIG 6 VOL I.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 73,396 hrs · 30,049 cycles

VANE AIR CONDITION COMPARTIMENT LT PACK N°2 INTERNAL SIDE STA 475 TEE P/N NCA6048-105 WITH CRACK 4 INCH. REPAIRED STIFFENER FOR SRM 53-40-00 FIG 10 VOL I.

Part: FRAME — CRACKED (ZONE 100) · airframe 73,396 hrs · 30,049 cycles

VANE AIR CONDITION LT SIDE STRUCTURE FRAME STA 535 DEFORMED AND CORROSION . SUSPECT SUPPORT FITTING CRACKED. PERFORMED NDI CHECK ON SUPPORT NO FOUND CRACK. REPAIRED SECTION FRAME FOR SRM 53-30-00 FIG 5 VOL I AND PROTECT FOR SRM 51-21-01 VOL II.

Part: FRAME — CRACKED (ZONE 200) · airframe 73,396 hrs · 30,049 cycles

DURING MD10 ACF MODIFICATION, FOUND CRACK 4,5" LONG ON THE FRAME AT STA 1781 TO STRINGER 13 LT PERFORMED REPAIR FOR SRM VOL I 53-30-00 FIG 5.

Part: FRAME — CRACKED (ZONE 200) · airframe 73,396 hrs · 30,049 cycles

DURING MD10 ACF MODIFICATION, FOUND CRACK 4.5" LONG ON THE FRAME AT STA 1801 TO NEXT STR 13 RT SIDE AND 2 RIVET MISSING ON THE SPLICE FO. PERFORMED REPAIR FOR SRM 53-30-00 FIG 5 VOL I. INSTALLED RIVETS FOR SRM 51-35-01.

Part: INTERCOSTAL — CRACKED (ZONE 600) · airframe 73,396 hrs · 30,049 cycles

MD10 TO ACF MODIFICATION FOUND RT WING TRAILING EDGE LOWER SIDE STA XORS 241 ABOUT INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL FOR SRM 51-35-01.

Part: FRAME — CRACKED (ZONE 200) · airframe 73,396 hrs · 30,049 cycles

DURING MD10 ACF MODIFICATION, FOUND CRACK 4" LONG ON THE FRAME STA 1821 TO NEXT STRG 11 LT SIDE REPAIRED FOR SRM 53-30-00 FIG 5 VOL I.

Part: FRAME — CRACKED (BS 421) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 ACF, FOUND IN AVIONIC COMPT, INTERNAL, STA 421 RT SIDE AT X=-77 ABOUT FRAME WITH CRACK 4,5" LONG REPAIRED FOR SRM 53-30-00 FIG 5 VOL I.

Part: FRAME — CRACKED (ZONE 200) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 ACF, FOUND ON FRAME AT STA 1741 TO NEXT STR 11 RT SIDE CRACK 4,5" LONG REPAIRED FOR SRM 53-30-00 FIG 5 VOL I.

Part: FRAME — CRACKED (ZONE 200) · airframe 73,396 hrs · 30,049 cycles

DURING MODIFICATION MD10 ACF, FOUND CRACK 4,5" LONG ON THE FRAME AT STA 1761 TO NEXT STRG 13 LT SIDE. REPAIRED FOR SRM 53-30-00 FIG 5 VOL I.

Part: TRANSPONDER — MALFUNCTIONED · airframe 71,930 hrs · 29,279 cycles

NR 1 TRANSPONDER READS 300-400 FT LOW AT FL 320. RELEASED FOR SERVICE PER MEL/CDL: 34-26-A CATEGORY: C EXPIRATION: 27JUN06 "MEL 34-26-A: NR 1 TRANSPONDER INOP." USING PITOT/STATIC BOX DROVE ALTITUDE TO 32K FOR BOTH AIR DATA COMPUTERS. CHECKED BOTH TRANSPONDERS AT DIFFERENT ALTITUDES, ALL INDICATIONS AND TRANSPONDER OUTPUTS CHECKED CORRECT. BOTH SYSTEMS DISPLAYED 32.0 AT 32,000. NO PROBLEMS NOTED WITH THE NR1 TRANSPONDER OR AIR DATA. ALL TEST CONNECTIONS WERE EXTERNAL. NO A/C LINES DISTURBED. RVSM STATUS REMAINS VALID. ALL WORK REF MM 34-54-00-5.

Part: PROXIMITY SENSOR — CONTAMINATED (RT MLG) · airframe 69,604 hrs · 28,077 cycles

UNSAFE INDICATION IN RIGHT MAIN LANDING GEAR LIGHT AFTER RAISING GEAR HANDLE ON TAKEOFF. MAINTAINED AIRSPEED, RAN QRH PROCEDURE, LIGHT WENT OUT AFTER CYCLING THE GEAR HANDLE. AIRCRAFT HAD REQUIRED DE-ICING AT MHT DUE TO SNOW STORM OVER THE PREVIOUS 24 HOUR. INSPECTED RT MLG PROXIMITY SENSORS AND FOUND TO BE COATED WITH DE-ICE FLUID. CLEANED PROX SENSORS ON RT MLG IAW SMP. PERFORMED BITE CHECK ON PROXIMITY ELECTRONICS UNIT IAW MM 32-61-01 WITH NO FAULTS NOTED, OK FOR SERVICE.

Part: HINGE — DAMAGED (ZONE 100) · airframe 69,161 hrs · 27,826 cycles

COMPLY WITH EA 8-5240-80594 DOORS SERVICE TAILCONE PATIO DOOR HINGE REPAIR P/N AKC7011 (RHS). COMPLIED WITH E/A/8-5240-80594.

Part: SUPPORT — CORRODED (TE FLAPS) · airframe 69,161 hrs · 27,826 cycles

COMPLY WITH EA 8-5750-80595 WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-80595, WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 69,161 hrs · 27,826 cycles

COMPLY WITH EA8-7120-79336 ENGINE MOUNTS ALIGNMENT PIN MINOR CORROSION REPAIR. COMPLIED WITH EA 8-7120-79336.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,161 hrs · 27,826 cycles

NR 3 AC BAY DOOR CTR VERTICAL FRAME CRACKED APPROX 12 INCHES FROM TOP OF DOOR. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-35-01 & SRM 51-33-01 AT MAE.

Part: NUT PLATE — DAMAGED (NR 3 NACELLE) · airframe 68,664 hrs · 27,552 cycles

ON LANDING ROLLOUT NR 3 WOULD NOT GO INTO REVERSE. DID NOT GET ANY LIGHTS FOR INDICATION OF REVERSE PRESS OR UNLOCK. BY DIRECTION OF MAINT TRIED TO CYCLE REVERSER ON TAXI IN, NO JOY. MEL 09APR04. RELEASED FOR SERVICE PER MEL/CDL: 78-01-01-A CATEGORY: A EXPIRATION: 03JAN07 MEL 78-01-01-A: ENGINE NR 3 THRUST REVERSER INOP. TAKEOFF PERFORMANCE PENALTY MAY APPLY. DO NOT REACTIVATE ENGINE NR 3 THRUST REVERSER WITHOUT PRIOR AUTHORIZATION FROM POWERPLANT ENGINEERING (REF AD CHECK NR 3 T/R TRANSCOWL DO NOT OPERATE TAG NUT PLATES. FOUND NUT PLATES BAD ON INBOARD AND OUTBOARD TRANSLATING COWL. REMOVED AND REPLACED NUT PLATES IN REF TO DC-10 SRM 51-31-01 VOL 2.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 68,234 hrs · 27,342 cycles

AFTER GEAR RETRACTION HAD RIGHT MAIN GEAR UNSAFE RED LIGHT ILLUMINATED ON FORWARD AND S/O PANEL. COMPLIED WITH QRH, CYCLED GEAR AND LIGHT WENT OUT. INSPECTED GEAR AND DOOR PER TAFI PG 109 32-30-00 AF. A/C OK FOR SERVICE.

Part: TRANSMITTER — FAILED (NR 3 ENGINE)

00-364 NR 3 ENGINE OIL TEMP GAGE MAXED OUT AT 200 DEG. SHUT DOWN NR 3 ENG IAW RED TAB PROC. RESECURED LOOSE CONNECTOR PLUG AND FAN COWLS.