N394FE

Part: SKIN — CRACKED (TE FLAP) · airframe 97,001 hrs · 37,620 cycles

LH WING OUTBOARD FLAP UPPER SURFACE SKIN HAS TWO CRACKS LOCATED AT THE INBOARD HINGE AREA 0000608631 : F - 01-NOV-2019 01:12 REPAIRED REF MD10 SRM 57-10-00 TRACKING EA 8-5750-T0350557 PART 1

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 96,652 hrs · 37,383 cycles

AFTER LANDING ROLLOUT, THE LEVEL 1 BRAKE DIFF TEMP ALERTED, FOLLOWED BY THE LEVEL II (2) BRAKE OVERHEAT. BRAKES 5 & 6 PEAKED AT APPROX 600, BRAKES 1 & 2 PEAKED AT JUST BELOW 500. BRAKES 3-4, 7 & 8 NEVER EXCEEDED 200. MINIMAL BRAKING WAS USED FROM LANDING ROLLOUT TO SHUT DOWN. FLAPS 35, LANDING WEIGHT 348K. T/S REF FIM 32-46-00-2-0. HOT BRAKES. INSPECTED TIRES AND BRAKES FOUND NO DISCREPANCYS. FUSE PLUGS WHERE INTACT WITH NO LEAKS. JACKED ACFT AXLE REF AMM 07-12-00-2-0. TIRES WHERE ROTATED FREELY WITH NO BINDING. SPINNING TIRES WHERE STOPPED UPON BRAKE APPLICATION. THEN ROTATED FREELY AFTER BRAKE WAS RELEASED. BRAKE SYS 1 AND SYS2 WHERE COMPRESSING AND RELEASING. COULD NOT FIND ANY DISCREPANCY AT THIS TIME. ACFT OK FOR SERVICE.

Part: PROBE — OUT OF LIMITS (FUEL TANK) · airframe 96,027 hrs · 36,966 cycles

PDIS 394 28-40 3649 18DEC18 BNA OPEN U LOGPAGES:2876587 NR 2 FUEL QUANTITY DECREASED DISPROPORTIONATELY WITH NR 1 & NR 3 TANKS. POSSIBLE FUEL LEAK, OR SENSOR MALF (PREVIOUS WRITE UP). FACT 23DEC18 01:09 IAH ALL THE WORK DONE SERVICE WORK ORDER #11834R2215 : TROUBLESHOT NR 2 FUEL QTY. IN REF: FIM 28-41-00-2, FOUND NR 3 PROBE ON LEFT AND RIGHT NR 2 TANK, NR 4 AND NR 5 PROBE RIGHT SIDE NR 2 TANK AND RIGHT MJP OUT OF LIMITS ALSO FOUND NR 3 PROBE HARNESS NIN NR 2 TANK SHORTED. REMOVED AND REPLACED NR 3 PROBE LEFT AND RIGHT SIDE NR 2 TANK, NR 4, NR 5 PROBE RIGHT SIDE NR 2 TANK IN REF: AMM 28-41-03-4. REMOVED AND REPLACED RIGHT MJP IN NR 2 TANK IN REF: AMM 28-41-02-2. REMOVED AND REPLACED NR 3 PROBE HARNESS LEFT SIDE NR 2 TANK IN

Part: CAP — DAMAGED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RT WING REAR UPPER SPAR AREA, APPROX XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAS SMALL AREA OF DAMAGE. REPAIRED PER EA 8-5710-T0342036 PART 1.

Part: RIB — DAMAGED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RIGHT WING, REAR UPPER SPAR AREA, XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAD A SMALL AREA OF DAMAGE. REPAIRED IAW EA 8-5710-T0342036.

Part: REPAIR — DAMAGED (TE FLAP VANE) · airframe 95,880 hrs · 36,890 cycles

LT I/B FLAP VANE, I/B END HAS A DAMAGED REPAIR ON TOP SKIN. REPAIRED DAMAGE ON LT I/B FLAP VANE, I/B END TOP SIDE, IAW SRM 51-71-00 VOL 2, PAR 16.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 95,880 hrs · 36,890 cycles

RT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL 1, FIG 7, AND SRM 51-31-01, VOL 2.

Part: SPAR — DAMAGED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RT WING LOWER REAR SPAR REQUIRES SR10570048-6 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER EA 8-5710-T0340000.

Part: SPAR — DAMAGED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RT WING LOWER REAR SPAR REQUIRES SR10570049-60 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000.

Part: SPAR — DAMAGED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RT WING LOWER REAR SPAR REQUIRES (2) SR10570048-38 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER ES 8-5710-T0340000.

Part: FRAME — CORRODED (FUSELAGE) · airframe 95,880 hrs · 36,890 cycles

CTR CARGO COMPT STA 1741 FRAME HAS CORROSION BY LONG 52. REMOVED AND REPLACED A SECTION OF CORRODED FRAME (CHANNEL) AT STA 1741 AT LONGERON 52 REF SRM 53-30-00 FIG 5 (SHEET 2) VOL I MAJOR REPAIR.

Part: FLAP SYSTEM — CRACKED · airframe 95,880 hrs · 36,890 cycles

REWORK REF N/R N00460 "LH WING ATTACH FITTING FOR O/B FLAP I/B HINGE HAS A .5 IN. CRACK ON THE O/B HALF AT THE FWD FASTENER. (MRKD)" REWORK PER QA REVIEW REJECTION. FITTING REPLACEMENT PART/MATERIAL NOT IDENTIFIED SNRM BLOCKS 23,24,25 AND NO RDR AND SDR GENERATED AS REQUIRED. FLAP HINGE SUPPORT STA.XW486.403 REPLACED WITH P/N# ARB2431-507

Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 95,880 hrs · 36,890 cycles

RIGHT WING OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING ON THE AIRCRAFT SIDE, FOUND CORRODED AT THE FASTENER HOLES. REMOVED THE CORROSION. REMOVED AND REPLACED THE SIDE LOAD FITTING IAW SRM 51-33-01, VOL II, & DWG ARB0031.

Part: SEAT TRACK — DAMAGED (BS 800) · airframe 95,880 hrs · 36,890 cycles

UPPER MAIN CARGO DECK LT SIDE, UNDER A BALLMAT AT BS 800, LBL 48 SEAT TRACK LOBE DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1.

Part: SKIN — CORRODED (LT WING) · airframe 95,880 hrs · 36,890 cycles

LEFT UPPER WING SKIN HAS CORROSION AT FASTENER, XORS 423. AFT OF FRONT SPAR. REPAIRED IAW EA 8-5730-T0339577-P1. REPAIR CLASSIFIED AS MINOR.

Part: RIB — CRACKED (RT WING LE) · airframe 95,880 hrs · 36,890 cycles

RIGHT WING L/E ACCESS PANEL 619DB, INSIDE UPPER RIB FLANGE IS CRACKED ABOVE PULLEY OTBD OF THE NR 10 SLAT TRACK.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 95,880 hrs · 36,890 cycles

LEFT WING NR 3 SPOILER TOP SKIN HAS MULTIPLE AREAS OF DELAMINATION. REPAIRED IAW SRM 51-71-00, VOL II, PAR 16.

Part: SHEAR TIE — CORRODED (BS 1950) · airframe 95,880 hrs · 36,890 cycles

AFT CARGO BAY, BS 1950, CORROSION ON THE FRAME SHEAR TIE BETWEEN LONGERONS 51 AND 52R. REPAIRED THE SHEAR TIE IAW SRM 53-30-00, PG 2, FIG 10, VOL 1.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 95,880 hrs · 36,890 cycles

RT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL I, FIG 7, SRM 51-31-01, VOL II.

Part: BEAM — CRACKED (BS 535) · airframe 95,880 hrs · 36,890 cycles

L3 DOOR, NR 1 BEAM AFT SIDE AT THE DOOR FRAME STOP WAS FOUND CRACKED. REMOVED AND REPLACED THE BEAM IAW DWG ADA 0006, AND SRM 51-31-01.

Part: BULKHEAD WEB — CRACKED (BS 595) · airframe 95,880 hrs · 36,890 cycles

BS 595 BULKHEAD, RT FWD SIDE OF WEB HAS A 1 INCH CRACK THRU FASTENER HOLE AT RBL 60, Z100.00. PERFORMED A BULKHEAD REPAIR IAW SRM 53-40-00, FIG 25 V1.

Part: SPAR CAP — CRACKED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RT WING REAR SPAR LOWER CAP AT XORS 446 HAS A 2.0 INCH CRACK AT THE AFT EDGE OF TEE CAP EXTENDING THROUGH THE RADIUS AND TERMINATING 1.0 IN UP THE VERTICAL LEG. REPAIRED PER EA 8-5710-T0340000.

Part: FRAME — CORRODED (BS 1741) · airframe 95,880 hrs · 36,890 cycles

CENTER CARGO BAY BS 1741 FRAME HAS CORROSION BY LONGERON 52. REPAIRED THE CORRODED FRAMED IAW SRM 53-30-00, VOL I, PAGE 31.

Part: WEB — CRACKED (NLG WW) · airframe 95,880 hrs · 36,890 cycles

NOSE LANDING GEAR WW, RT SIDE FWD OF INNER WEB, BS 495, Z-65. CRACKED FROM FASTENER HOLES. REPAIRED IAW SRM 53-30-00, FIG 6, SH 8, VOL I. MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RT WING SKIN AT THE INBOARD UPPER CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT HAS A .500 INCH CRACK PROPAGATING THROUGH AN EXISTING STOP DRILL. INSTALLED A REPAIR DOUBLER PER SRM 57-10-00 FIG 103.

Part: SPAR CAP — CRACKED (RT WING) · airframe 95,880 hrs · 36,890 cycles

RT WING REAR SPAR LOWER CAP AT XORS 421 HAS A .200 INCH CRACK PROPAGATING FWD OF A PREVIOUS TRIM OUT REPAIR AND EXTENDING INTO THE RADIUS. REPAIRED PER EA 8-5710-T0340000.

Part: CARGO TRACK — GOUGED (BS 879) · airframe 95,880 hrs · 36,890 cycles

MAIN CARGO TRACK BS 879, RBL 8.5 GOUGED OUT OF LIMITS. REPLACED THE CARGO TRACK SRM 53-70-00, FIG 1, VOL 1.

Part: CARGO TRACK — DAMAGED (BS 635) · airframe 95,880 hrs · 36,890 cycles

MAIN CARGO TRACK BS 635 RBL 27.5 DAMAGED BEYOND LIMITS. REPAIRED THE TRACK IAW SRM 53-70-00, FIG 1, VOL 1.

Part: CARGO TRACK — WORN (BS 859) · airframe 95,880 hrs · 36,890 cycles

MAIN CARGO BAY, BS 859, LBL 107.25 SEAT TRACK IS WORN OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1.

Part: CAP — CRACKED (BS 595 BULKHEAD) · airframe 95,880 hrs · 36,890 cycles

RIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A .100 INCH CRACK THROUGH THE LOWER FASTENER HOLE. PERFORMED A TEE CAP REPAIR IAW DWG SR10530064.

Part: CAP — CRACKED (BS 595 BULKHEAD) · airframe 95,880 hrs · 36,890 cycles

LEFT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 41L HAS A 1 INCH CRACK THROUGH THE LOWER FASTENER HOLE. REPAIIRED THE TEE CAP IAW EA 8- 5310-T0339305 P1/P2. REPAIR CLASSIFIED AS MAJOR.

Part: SENSOR — OUT OF ADJUST (SLAT SYSTEM) · airframe 95,859 hrs · 36,876 cycles

AFTER SELECTING FLAPS 35 ON FINAL AT ORD GOT SLAT DISAGREE ALERT. DUE TO TIME LAG BETWEEN SELECTING FINAL FLAPS AND ALERT ELECTED, A SECOND APPROACH IN NORMAL CONFIGURATION. NO DISAGREE, BUT SUSPECT LIMIT INDICATORS ARE OUT OF ADJUSTMENT. FOUND R2B SLAT SENSOR INDUCTANCE READING LOW 5.431. NEAR, ADJUSTED THE R2B SENSOR TO 5.606/NEAR IAW MM 27-84-02. OPS CHECKED GOOD.

Part: LEVER — BINDING (R1 DOOR) · airframe 95,000 hrs · 36,380 cycles

R1 ARMING LEVER VERY DIFFICULT TO MOVE, FEELS LIKE CABLE IS STRETCHING RATHER THAN PARTS ARE MOVING.

Part: WIRE HARNESS — DAMAGED (NR 2 ENGINE) · airframe 94,955 hrs · 36,356 cycles

DURING CLIMBOUT, NOTICED THE NR 2 ENGINE EXCEEDENCE LEVEL 1 ALERT. EGT GAUGE FOR NR 2 SHOWED MAX 998. NORMAL EGT AT REDUCED POWER FOR LEVEL FLIGHT AT 7000 FT. ON ADVANCING POWER FOR CLIMB, NR 2 EGT CLIMBED RAPIDLY. PERFORMED GVI OF THE VSV FEED BACK CABLE AND STATIC RIG CHECK POINTS IAW MM 73-20-01-2, FIG 202, NO DEFECTS NOTED. REMOVED AND REPLACED ALL NR 2 ENGINE EGT THERMOCOUPLE HARNESSES AND PERFORMED ADJUSTMENT AND TEST MM 77-21-01-2. REQUIRES ENGINE RUN FOR OP CHECK.

Part: SEAT TRACK — DAMAGED (BS 1388) · airframe 93,670 hrs · 35,665 cycles

SEAT TRACK FOUND DAMAGED BS 1388 RBL 75.25. REPAIRED IAW SRM 53-70-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 93,670 hrs · 35,665 cycles

REPORTS A LOCK AT STA 1400, LOCK IN MAIN DECK CARGO IS NOT SECURE. PRIOR TO DEPARTURE, DISCOVERED SEAT TRACK DAMAGED WHERE LOCK IS LOCATED. NO DAMAGE TO LOCK WAS INDICATED. RELEASED FOR SERVICE IAW MEL: 25-57-02-A2, CATEGORY: A, EXPIRATION: 12OCT16, MEL 25-57-02-A2. RESTRAINT INOPERATIVE. REPAIRED SEAT TRACK IAW SRM 53-70-01, FIG 1, SPLICED IN NEW SECTION OF SEAT TRACK.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,073 hrs · 35,341 cycles

CENTER CARGO AREA LT SIDE AT BS 1781, STRINGER 43L HAS CORROSION. R & R THE LONGERON END CAP IAW SRM 51-31-01 VOL 2. FABRICATED NEW LONGERON END CAP ON T16 1202867, PN AFA3275-501 IAW SRM 53-15-01 PG 8B & 9 VOL 3. MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 93,073 hrs · 35,341 cycles

CENTER WING UPPER SKIN AT STATION 1297, LBL 84 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL 1. INSPECTED AREA IAW NTSPM 06-10-01 & 06-00-03. NO DISCREPANCIES NOTED. COMPLIED WITH EA 8-5730-T0324785, CTR WING BOX, UPPER SURFACE CORROSION REPAIR 5 PLACES. MINOR REPAIR.

Part: SKIN — CORRODED (FUEL TANK) · corrosion level 2 · airframe 93,073 hrs · 35,341 cycles

TOP SURFACE OF CTR WING TANK AT STATION 1224, LBL 90 - 105 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL II FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL I. INSPECTED AREA IAW NTSPM 06-10-01 & 06-00-03. NO DISCREPANCIES NOTED. COMPLIED WITH EA 8-5730-T0324785. CTR WING BOX UPPER SURFACE CORROSION 5 PLACES. MINOR REPAIR.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 93,073 hrs · 35,341 cycles

CENTER WING UPPER SKIN AT 1298, LBL 95, HAS CORROSION. REMOVED 6 EACH FASTENERS IAW SRM 51-30-01, VOL 2. REMOVED CORROSION IAW SRM 51-21-01 VOL 2. CHECKED LIMITS, ORIGINAL MATERIAL = .220, REMAINING MATERIAL = .182. FOUND OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL 1. COMPLIED WITH EA 8-5730-T0324785, CTR WING BOX UPPER SURFACE CORROSION, REPAIRED 5 PLACES. MINOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 93,073 hrs · 35,341 cycles

TWO EACH DENTS ON UPPER FUSELAGE, EXTERNAL SURFACE AT FS 401, CLOSE TO L1 DOOR. COMPLIED WITH EA. 8-5330-T0324851 PT 1, DENTS AT FS 401 FWD OF L1 DOOR. APPLIED DENT DOT IAW GMM 06-3-101.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 93,073 hrs · 35,341 cycles

FLOORBEAM CRACKED AT STATION 1801, LBL 54 AT AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM IAW SRM 53-60-01 FIG 3 VOL 1. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 93,073 hrs · 35,341 cycles

MAIN DECK AREA STATION 775, BL 0 FLOOR PANEL PUNCTURE. FABRICATED REPLACEMENT PANEL ON T16 1202347 IAW DWG SRZ-25-005. R & R FLOOR PANEL IAW 53-21-08-04, MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 93,073 hrs · 35,341 cycles

GOUGES & MINOR DAMAGES ON SEAT TRACK SCALLOPS AT MAIN DECK CARGO COMPARTMENT, LBL 8.5 LT, BETWEEN FS 1521 & 1621. R & R SEAT TRACK AT LBL 8.5, FROM STATION 1531 - 1631, IAW SRM 51-01-01 VOL II, ON MAIN DECK CARGO, MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 93,073 hrs · 35,341 cycles

FLOORBEAM AT STATION 1821, HAS A CRACK AT LBL 54, INBD OF AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM AT STATION 1821, LBL 54 IAW SRM 53-60-01 FIG 3 VOL 1 MAJOR REPAIR.

Part: STRAP — DEFECTIVE (COCKPIT) · airframe 93,073 hrs · 35,341 cycles

BOTH THE CAPTAIN & FIRST OFFICER ESCAPE STRAPS DO NOT REACH THE GND, AS REQUIRED BY STEPS 2 B 3 & 3 B 3 OF WC 25C6503. R & R CAPTAINS & FIRST OFFICERS ESCAPE STRAPS. OPERATIONS CHECKED GOOD IAW AMM 25-60-01-2.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 92,771 hrs · 35,185 cycles

R1 DOOR PNEUMATIC PSI TEST FAILED. RELAMPED WITH CORRECT LIGHT BULBS. OPERATIONS CHECKED NORMAL IAW AMM 25-61-03-5-0.

Part: SWITCH — INTERMITTENT (PAX DOOR) · airframe 916 hrs · 34,510 cycles

LEFT ENTRY DOOR FAILS TO MOVE UP OR DOWN, STUCK IN MID POSITION. DOOR SWITCH INTERMITTENT INTERIOR & EXTERIOR. REPLACED OPEN/CLOSE SOLENOID. ADJUST AND TEST CHECKS GOOD. IAW AMM 52-11-00-5 & 52-11-13-2.

Part: SKIN — CRACKED (LT WING) · airframe 90,676 hrs · 33,950 cycles

POSSIBLE CRACK FOUND ON LT WING AFT BOTTOM SIDE SKIN BY NR 1 SLAT CTR TRACK PANEL. SLATS EXTENDED FOR SHEET METAL REPAIR ACCESS, CB FOR AUX PUMPS ON BACK WALL PULLED & COLLARED. PERFORMED HFEC TO VERIFY CRACK IAW NTM PT 6. REMOVED THE NR 1 SLAT IAW MM 27-80-01-4 FOR FOM. TRIMMED DAMAGED AREA. CHECK CUT OUT AREA TO VERIFY ALL CRACK WAS REMOVED & DISCARDED IAW NDT SPM 06-10-01. NO EVIDENCE OF CRACK WAS FOUND. FABRICATED DOUBLER IAW SRM VOL 57-10-00 FIG 68 EA 8-5710 T0308395. REPAIRED LT LE SKIN AT SLAT TRACK 2 CUT OUT IAW EA 8-5710-T0308395.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 90,565 hrs · 33,893 cycles

DURING EMERGENCY LIGHT OPS CHECK, NO EMERGENCY LIGHTS ILLUMINATED, COCKPIT OR CABIN, EXCEPT EXIT SIGNS. TROUBLESHOTIAW SSM 33-51-0 & DM 33-52-01. FOUND NO VDC AT PIN 2 ON TERMINAL BLOCK S3 - 692 WITH EMERGENCY LIGHT ON. DISCONNECTED ALL WIRE AT PIN 2 & FOUND 28VDC AT WIRE 1257-20. CONNECTED ALL OTHER WIRES, ALL WORKING EXCEPT LT FWD DOOR EMERGENCY LIGHT. REPLACED LAMPS ON LT FWD DOOR EMERGENCY LIGHT, ALL WORKING PROPERLY. EMERGENCY LIGHT FUNCTIONAL CHECK OUT IAW AMM 33-50-00-5.

Part: BRACKET — CORRODED (FWD CARGO) · airframe 90,529 hrs · 33,872 cycles

FORWARD LOWER CARGO BAY SIDE GUIDE BRACKET HAS CORROSION. REMOVED CORRODED BRACKET AND INSTALLED NEW BRACKET AS PER SRM 51-31-01 VOL. II.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 90,529 hrs · 33,872 cycles

DURING C CHECK, FOUND RT HORIZONTAL STABILIZER UPPER FWD PLANK, APPROXIMATELY 28 INCHES OTBD OF BULKHEAD, CRACKED APPROXIMATELY 2 INCHES IN LENGTH. REPAIRED IAW SRM 55-20-00 FIG. 10 AND EA. 8-5510-T0306782.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 90,529 hrs · 33,872 cycles

RT HORIZONTAL UPPER AFT PLANK SKIN OTBD OF CTR BOX SECTION HAS 3 INCH CRACK. REPAIRED IAW EA 8-5510-T0306750 P1.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 90,529 hrs · 33,872 cycles

RT HORIZONTAL STABILIZER, UPPER FWD PLANK APPROXIMATELY 26 INCHES OTBD FROM CONTROL BOX SECTION HAS 1.25 INCH CRACK. REPAIRED IAW EA 8-5510-T0306782.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,300 hrs · 33,758 cycles

EMERGENCY LIGHTS WILL NOT COME ON. ACCOMPLISHED ADJUSTMENT TEST IAW AMM-33-50-00-5. OK FOR CONTINUED SERVICE.

Part: BATTERY PACK — INOPERATIVE (R1 DOOR SLIDE) · airframe 90,063 hrs · 33,630 cycles

R1 DOOR SLIDE PUSH TO TEST SWITCH DOES NOT TEST. TWO NEW BATTERIES INSTALLED IN R1 DOOR SLIDE BATTERIES PACK IAW AMM 25-61-01-2. PTT SWITCH TEST CUT OUT, SERVICEABLE.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 89,933 hrs · 33,565 cycles

ENROUTE AT FL310, HYD SYS 1 FAILED. FLUID IN NR 1 HYD SYS FELL TO 2.5 GALS , PUMPS TURNED OFF. FOUND NR 1 HYD SYS MANIFOLD PRESSURE LINE B-NUT AND UNION LOOSE AND LEAKING. TIGHTEN AND TORQUED BOTH REF AMM 29-12-07-2 AND AMM 20-50-01. NO LEAKS NOTED, SERVICED SYS AS REQUIRED REF AMM 12-13-02-3 .

Part: WEB — CRACKED (MLG WW) · airframe 87,975 hrs · 32,509 cycles

CENTER MLG WHEEL WELL, LT SIDEWALL LIGHTNING HOLE IS CRACKED AT BS 1391, LBL 32. ACCOMPLISHED SPLICE AND DOUBLER REPAIR IAW EA 8-5710-156968.

Part: RIB — CRACKED (CTR WING) · airframe 87,975 hrs · 32,509 cycles

CENTER WING SECTION HAS A DAMAGED RIB. REPAIRED IAW EA 5710-156972.

Part: SPAR CAP — CRACKED (ZONE 500) · airframe 87,975 hrs · 32,509 cycles

LEFT WING REAR SPAR LOWER CAP AT WING STA XORS 347.750, THREE FASTENER HOLES FOUND CRACKED IAW NDT SPM PART 06. COMPLIED REPAIR IAW EA 8-5710-156957, REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 87,975 hrs · 32,509 cycles

FUSELAGE IS PUNCTURED BETWEEN FRAME STA 808 AND 824 , L44R TO L45R. REPAIRED FUSELAGE SKIN IAW SRM 53-20-00, FIG 6, REPAIR CUT OUT HFEC IAW NTSPM 06-10-01.

Part: SKIN — MISREPAIRED (BS 1480) · airframe 87,975 hrs · 32,509 cycles

LOWER BELLY FUSELAGE (UNDERWING BARREL) SKIN AT STA1480 ON CENTERLINE HAS AN UNAPPROVED REPAIR FOR THE SPECIFIC AREA IAW EO E8-5100-7-5001 PT 1 CRITERIA. REPAIRED LOWER BELLY FUSELAGE SKIN BY INSTALLING NEW REPAIR DOUBLER IAW SRM 53-40-00, FIG 20 AND SRM 51-31-01, FIG 20, SH 2.

Part: SEAT TRACK — WORN (UPPER CARGO) · airframe 87,975 hrs · 32,509 cycles

CARGO TRACK AT LBL 77.5, BS 1391 TO 1401 HAS 2 LOBES WORN. BLENDED AREA IAW SRM 53-70-00, CHECKED LIMITS: ORIG. MAT. 0183" MAT LOSS .043". FOUND TO BE OUT OF LIMITS IAW 53-70-00. FABRICATED CARGO TRACK IAW STAM TRAVELER T12/923517 , R & R SEAT TRACK IAW SRM 51-31-01.

Part: SKIN — MISREPAIRED (BS 1721) · airframe 87,975 hrs · 32,509 cycles

FOUND SKIN AT FS 1721 BETWEEN S46 TO 48L MISREPAIRED. REPAIRED SKIN IAW SRM 53-20-00, FIG.6, REPAIR IS CLASSIFIED AS MAJOR.

Part: PULLEY — WORN (R1 DOOR FRAME) · airframe 87,975 hrs · 32,509 cycles

R-1 DOOR UPPER AFT DOOR JAMB DOOR CABLE PULLEY IS WORN. R & R PULLEY ASSY IAW SRM 51-31-01. RIG NOT DISTURBED AND OPS CHECKED GOOD IAW AMM 52-11-00-5.

Part: CARGO TRACK — WORN (BS 753-760) · airframe 87,975 hrs · 32,509 cycles

CARGO TRACK AT FS 753 TO FS 760 AT BL47.5L HAS 3 EA WORN LOBES. R & R MAIN DECK CARGO TRACK BETWEEN FS 753 TO FS 760 AT BL47.5L IAW SRM 53-70-00, REPAIR IS CLASSIFIED AS MAJOR.

Part: PULLEY — WORN (L1 DOOR FRAME) · airframe 87,975 hrs · 32,509 cycles

L1 DOOR AFT DRIVE CABLE, UPPER DOOR FRAME PULLEY WORN. R & R PULLEY ASSY IAW SRM 51-31-01. NO RIG DISTURBED AND OPS CHECKED GOOD IAW AMM 52-11-00-5.

Part: FLOOR PANEL — CORRODED (BS 1975) · corrosion level 3 · airframe 87,502 hrs · 32,267 cycles

SEVERAL RIVET HEADS MISSING FROM AFT FUSELAGE LT SIDE. MARKED AREAS WITH TAPE. REMOVED 1 FLOOR PANEL IN BULK PIT FOR ACCESS. PANEL LT IN BULK PIT. APPLICABLE SRM CORROSION REPAIRS.

Part: ANTI-SKID SYS — FAILED (ZONE 100) · airframe 87,028 hrs · 32,012 cycles

AFTER DROPPING THE GEAR FOR LANDING GOT LEVEL 2 "ANTI-SKID L FAIL". DID AN ANTI-SKID TEST AND ALERT RETURNED. WENT AROUND & RAISED GEAR. ON NEXT APPROACH, DID NOT GET THE ALERT. NORMAL LANDING, R & R ANTI-SKID CONTROL UNIT IAW AMM 32-45-01-4. RTS TEST PASSED. NO FAULTS NOTED AT THIS TIME.

Part: WIRE — BURNED (COMPASS) · airframe 86,548 hrs · 31,751 cycles

STANDBY COMPASS POWER CABLE POPPED, SMOKED AND BURNED THRU WHEN STANDBY COMPASS LIGHT WAS SELECTED. FOUND LIGHT RECEPTACLE PULLED FROM REAR OF STBY COMPASS. WRAPPED AND SECURED WIRE. STBY COMPASS LIGHT C/B D-13 PULLED AND COLLARED.

Part: BOTTLE — DISCHARGED (EMERGENCY ASSIST) · airframe 86,468 hrs · 31,708 cycles

ON PREFLIGHT F/O FOUND L1 DOOR EMERGENCY BOTTLE DISCHARGED. RESET L1 DOOR EMERGENCY ASSIST SYS AND RECHARGED L1 DOOR ACCUMULATOR IAW MM 52-10-01-2-0. OP'S CHECK NORMAL.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 85,616 hrs · 31,259 cycles

AIR MANIFOLD 2 FAIL. AFTER FLAP RETRACT ON TAKEOFF. MOVED THROTTLE TO IDLE IAW QRH. DUMPED FUEL AND RETURNED TO DEPARTURE. PERFORMED DECAY CK OF NR 2 PNEU SYS IAW MM 36-00-01-5 TIME WAS 25 SEC. FROM 20 TO 15 PSI. DECAY CK GOOD. THE MANIFOLD FAIL WAS ON STATICLY WITH NO AIR LOAD AND LOW DUCT TEMP. PERFORMED ADJUSTMENT TEST AND AND THE CONTROLLER FAILED. R & R NR 2 MANIFOLD FAIL CONTROLLER IAW MM 36-23-01-5. AWAITING TDR.

Part: CONTROL VALVE — FAILED (TE FLAPS) · airframe 85,616 hrs · 31,259 cycles

ON FLAP RETRACT AFTER TAKEOFF. WITH FLAPS 0 SLAT EXT GOT FLAP DISAG ALERT. ATTEMPTED TO EXTEND FLAPS BACK TO 15 & FLAPS WOULD NOT MOVE. FLAPS INDICATED EXT/0. DUMPED 20,000 LBS OF FUEL & MADE 0/EXT LANDING. TOUCHDOWN AT 174 KTS. WEIGHT 362,000. T/S FLAP SYS REF FIM 27-50. INTERROGATED CFDS FCC 1 & 2 ALL 3 VIAS & ALL 3 AIU'S WITH NO FAULTS FOUND. PERFORMED RTS ON ALL ABOVE WITH NFF. PERFORMED OPS CHECK OF FLAP SYS. SYS OPERATES SMOOTHLY. RAN FLAPS 7 COMPLETE CYCLES WITH ALL INDICATIONS NORMAL. REMOVED LT & RT OTBD FLAP POS TRANSMITTER PANELS 535 BR & 625 BR. VISUALLY INSPECTED MECHANISMS. NO DEFECTS NOTED. R & R INBD FLAPS CONTROL VALVE & ASSOCIATED RESTRICTORS & CHECK VALVES. LEAK CHECKS GOOD. REF MM 27-52-02-2. PERFORMED ADJUSTMENT TEST OF INBD FLAP CONTROL VALVE REF MM 27-52-02-2. NO DEFECTS NOTED AT THIS TIME. PERFORMED OPS TEST OF FLAP HYD ACTUATION SYS NO DEFECTS NOTED REF MM 27-50-00. RII FOR INSTALL OPS & LEAK CHECK. AWAITING TDR RESULTS.

Part: SKIN — DAMAGED (ZONE 100) · airframe 85,606 hrs · 31,248 cycles

FUSELAGE, LT SIDE AFT OF AFT PIT DOOR, APPROX AT STA 1853 TO STA 1902, BETWEEN L38 TO L39 HAS 2 EA 10 INCHES CREASED IN SKIN. REPAIRED SKIN WITH DOUBLERS INSTALLATION IAW SRM 51-31-01, AND SRM 53-20-00, MAJOR REPAIR.

Part: SKIN — GOUGED (BS 1801 L36R) · airframe 85,606 hrs · 31,248 cycles

RT FUSELAGE, AFT OF CTR PIT DOOR APPROX STA 1801, BELOW L36 HAS 2 GOUGLES. CUT OUT DAMAGE IAW SRM 53-20-00, FIG 16-6, FABRICATED REPAIR DOUBLERS IAW SRM 53-20- 00 AND INSTALLED ALL REPAIR PARTS IAW SRM 53-20-00 AND SRM 51-31-01, MAJOR REPAIR.

Part: SKIN — GOUGED (BS 1781 L28R) · airframe 85,606 hrs · 31,248 cycles

RT FUSELAGE, AFT OF CTR CARGO DOOR , APPROX STA 1781 AT HINGE LEVEL, L-28 HAS CREASE IN SKIN FWD OF PREVIOUS REPAIR. REPAIRED SKIN IAW SRM 53-20-00, FIG 6 WITH DOUBLERS AND FILLERS AS REQUIRED, MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 85,606 hrs · 31,248 cycles

FWD PIT SHEAR TIE IS CORRODED AT STA. 899 BETWEEN S-50R TO S-51R. REMOVED AND REPLACED FWD PIT SHEAR TIE AT STA. 899 BETWEEN S-50R TO S-51R IAW SRM 51-31-01, MAJOR REPAIR.

Part: SKIN — CORRODED (WING BOX) · airframe 85,606 hrs · 31,248 cycles

CTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 73 TO LBL 38, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, LBL 73-LBL38 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (WING BOX) · airframe 85,606 hrs · 31,248 cycles

CORROSION AT FASTENER IN UPPER SURFACE OF CTR WING BOX, FS 1222 LBL75. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1222 LBL 75 AND COMPLIED WITH EA 8-5730-139141.

Part: SKIN — CORRODED (WING BOX) · airframe 85,606 hrs · 31,248 cycles

CTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -RBL 106 TO RBL 73, FS 1332 TO 1365. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1332-1365, RBL 106-73 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (WING BOX) · airframe 85,606 hrs · 31,248 cycles

CTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 106 TO LBL 73, FS 1332 TO 1365. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1332-1365, LBL 106-73 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (WING BOX) · corrosion level 2 · airframe 85,606 hrs · 31,248 cycles

CTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -RBL 106 TO RBL 73, FS 1300 TO 1332. REMOVED CORROSION BY BLENDING. REMOVED 11 EA FASTENERS CHECKED LIMITS IAW EA8-5730-139141 AND REINSTALLED FASTENERS IAW SRM 51-31-01 AND EA 8-5730-139141 AT STA 1300-1332, LBL 73-LBL38. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (BS 1300-1332) · airframe 85,606 hrs · 31,248 cycles

CTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 38 TO LBL 0, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, LBL 38-0 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (WING BOX) · airframe 85,606 hrs · 31,248 cycles

CTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 106 TO LBL 73, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, LBL 106-73 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (WING BOX) · corrosion level 2 · airframe 85,606 hrs · 31,248 cycles

CTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -RBL 73 TO RBL 38, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, RBL 73-RBL38 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (WING BOX) · airframe 85,606 hrs · 31,248 cycles

CORROSION AT FASTENER IN UPPER SURFACE OF CTR WING BOX, FS 1289, LBL93. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1289, LBL 93 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 85,606 hrs · 31,248 cycles

RT OTBD FLAP, OTBD HINGE FLAP SIDE PIVOT BORES HAS PITTING CORROSION. REPAIRED IAW EA 8-5750-139132 WITH REPAIR BUSHINGS, MAJOR REPAIR.

Part: LONGERON — CORRODED (BS 1039) · airframe 85,606 hrs · 31,248 cycles

FWD PIT, STA 1039 AT RBL 51 HAS CORROSION AT AROUND AND UNDER FASTENERS AT PREVIOUS BLEND OUT AREA. REPAIRED FWD PIT AT STA 1039 AT RBL 51 STRINGER IAW SRM 53-10-00, FIG 2, MAJOR REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 85,606 hrs · 31,248 cycles

UPPER CARGO COMPARTMENT SEAT TRACK FROM FS 1391 TO FS 1399 AT LBL 77 HAS 2 EA WORN LOBES. R & R SEAT TRACK SEGMENT FROM FS 1301 TO FS 1399 AT LBL 77 IAW SRM 53-70-00 AND SRM 51-31-01, MAJOR REPAIR.

Part: PSEU — FAILED (SLATS) · airframe 85,481 hrs · 31,181 cycles

PASSING FL 16000 FT PSEU FAIL, SLAT DISAGREE AND OVERSPEED SLAT WARNING IAS 280KTS. RAN QRH LANDED KMKE 22/RET SLAT SENSOR 4A ON RT WING IS SHORTED WITH THE NAV LIGHT PWR SUPPLY. WIRES ARE SHORTED INSIDE A PLASTIC SECTION OF CONDUIT. VERIFIED THAT THE NAV LIGHT PWR SUPPLY WAS INDUCING THE VOLTAGE BY DESELECTING NAV LIGHTS. REWIRED PER WDM 27- 84-01 AND 33-44-01. R&R PSEU IAW AMM. OPEN

Part: SMOKE DETECTOR — FAULTY (CABIN) · airframe 77,274 hrs · 27,323 cycles

AT FL 360 GOT LVL 3 CABIN SMOKE ALERT (ONE OF THE MID CABIN 7 OR 8). DECLARED EMERGENCY, AND DIVERTED INTO KTUL. MEL. MAIN DECK CENTERLINE SMOKE DETECTORS INOP. DISPATCH PER MEL 27-17-01-03 A NR 2 CENTER SMOKE DET INOP SMOKE DET C/P DISCONNECTED AND STOWED. REMOVED AND REPLACED NR 2 SMOKE DETECTOR PER M/M 26-15-01-4 & TESTED PER 26-15-01-5.

Part: ENGINE — STALLED (NR 2) · airframe 77,215 hrs · 27,284 cycles

ENGINE NR 2 COMPRESSOR STALLS (SIGNIFICANT BANG-BANG) UPON THROTTLE REDUCTION, FL280- PERFORMANCE ENG SHUTDOWN PER QRH.

Part: ENGINE — VIBRATION (NR 2) · airframe 77,008 hrs · 27,177 cycles

ON TAKEOFF NR 2 THROTTLE REQUIRED ONE KNOB WIDTH BEYOND 1 & 3 ON CLIMBOUT AT 3000 FT AGL RECEIVED AIR MANF 2 FAIL WITH NOTICEABLE AIRFRAME VIBRATION. ENG 2 OIL TEMP HIGH ALERT FOLLOWED WITH PEAK OIL TEMP OF 201 DEGREES C. ENGINE WAS SHUTDOWN AND NR 2 ENGINE FIRE EXTINGUISHER DISCHARGED. INSPECTED INLET AND FOUND BIRD STRIKE DAMAGE. BORESCOPED FOUND SREVICABLE.REPLACED 2EA DAMAGED FAN BLADES, REPAIRED 11 EA BLADES, PERFORMED VIBE SURVEY AND TRIM BALANCE. REPLACED 6 FAN LINER SEGMENTS, REPEAIRED 2 HOLES IN THE COWLING. FOUND BAD OIL TEMP SENSOR,REPLACED. REPLACED RT BELLMOUTH ASSY DO TO DAMAGE AND REPLACED A DAMAGED FUEL LINE SWEDGE, LEAKING FUEL. OK FOR SERVICE.

Part: CONNECTOR — LOOSE (NR 1 ENGINE) · airframe 76,417 hrs · 26,882 cycles

AFTER SETTING MAX PWR AND ABOVE 90 KTS T/O ROLL RECEIVED ENG FAIL LIGHT, NR 1 ENG ROLLED BACK. REJECTED T/O. FOUND FIREWALL CONNECTOR NR P1-8002 NOT PROPERLY SECURED ON THE NR 1 PYLON. INSPECTED PLUG, NO DEFECTS NOTED. SECURED CONNECTOR. OPERATED ENGINE NR 1 TO TAKEOFF TARGET N1 ENGINE CHK GOOD. CHECKED CDP FOR CRACKS AND LEAKS, NONE FOUND. ENG'S READINGS WAS DOWNLOADED FROM FLT DATA RECORDER. ADJ PART POWER TRIM ON MEC FOR NR 2 ENG, DUE TO IT BEING HIGH. MAX POWER ASSURANCE WAS PERFORMED ON NR 1 AND NR 2 ENG. READINGS NORMAL. OK TO CONTINUE. REMOVED AND REPLACED NR 1 ENG FUEL FILTER . NO CONTAMINATES NOTED. RAN ENG, NO LEAKS NOTED. HIGH SPEED TAXI PERFORMED BY FLT CREW. ALL PARAMETERS WERE G

Part: ACTUATOR — LEAKING (RT MLG DOOR) · airframe 75,112 hrs · 26,199 cycles

AFTER T/O LAX, RT MAIN GEAR INDICATED UNSAFE AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY INDICATORS. RECYCLED PER QRH, NO CHANGE. DUMPED FUEL AND RETURNED FOR UNEVENTFUL LANDING. CHECKED: BUNGEE CYLINDER, EXTENSION RETRACTION ADJUSTMENT TEST, TARGET AND PROXIMITY SENSOR GAPS, BLED TRIM CYLINDER, TRUCK PIVOT RELATIVE MOVEMENT, LUBED GEAR, REPLACED RT GEAR DOOR ACTUATOR FOR BY-PASSING AND LEAKING. ALL ACCOMPLISHED AS PER MM. TEST FLEW AIRCRAFT WITH 3 LANDINGS. OK RETURNED TO SERVICE.

Part: ACTUATOR — INTERMITTENT (RT MLG) · airframe 75,077 hrs · 26,180 cycles

ON T/O, GEAR RETRACTION, RT GEAR LIGHTS REMAINED RED ON BOTH GEAR PANEL AND ON CONFIGURATION PAGE. RAN QRH PROCEDURE, DUMPED FUEL, RETURNED TO PDX, WHEN GEAR LOWERED, RECEIVED TWO IMMEDIATE GREEN LIGHTS FOR THE RT GEAR.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 75,692 hrs · 26,484 cycles

HORIZONTAL STABILIZER - CONSTANT SECTION SKIN PANEL CRACKED. PANELS REPLACEMENT PER SB 55-16.