N960DN

Part: WEB — CRACKED (WING) · airframe 53,648 hrs · 28,336 cycles

DUE A CRACK ON WEB, REMOVE AND INSTALL JACKSCREW GIMBAL ASSEMBLY. JACKSCREW ASSY WAS REMOVED AND INSTALLED.

Part: INTERCOSTAL — CORRODED (BS 1268-1288) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE INTERCOSTAL OVER LONGERON 29L, BETWEEN BS 1268 - 1288 IN THE AFT CARGO. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-05, VOL 2, AND DWG 9936632-9, REV S.

Part: LONGERON — CRACKED (BS 1364) · airframe 53,648 hrs · 28,336 cycles

CRACKED LONGERON 5R, AT BS 1364. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, FIG 7.

Part: LONGERON — CRACKED (BS 1364) · airframe 53,648 hrs · 28,336 cycles

CRACKED LONGERON 6R BS 1364. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, FIG 7.

Part: LONGERON — CRACKED (BS 1364) · airframe 53,648 hrs · 28,336 cycles

CRACKED LONGERON 4R, BS 1364. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, FIG 7.

Part: INTERCOSTAL — CORRODED (BS 750-769) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE INTERCOSTAL, LONGERON 29L, BETWEEN BS 750 - 769. THE INTERCOSTAL WAS REPLACED IAW DWG 9936632, REV J, AND SRM 51-30-05, VOL II.

Part: FRAME — CRACKED (BS 1520) · airframe 53,648 hrs · 28,336 cycles

CRACKED FRAME WEB AT AFT ACCESSORY BAY, BS 1520, CANT BETWEEN 10 AND 11 HRS POSITION, WEB AND DOUBLER WERE REPLACED IAW SRM 53-10-04 FIG 12 VOL III, 51-30-2 AND 51-30-5 VOL II. (LP# 0711110)

Part: SKIN — CRACKED (BS 1475) · airframe 53,648 hrs · 28,336 cycles

CRACK FOUND ON THE AFT ACCESSORY BAY INTERNAL SKIN AT BS 1475, BETWEEN LONGERONS 1L AND 2L. THE SKIN WAS REPAIRED IAW SRM 53-30-01, FIGURE 14, VOL I.

Part: FRAME — CRACKED (BS 1364) · airframe 53,648 hrs · 28,336 cycles

CRACKED FRAME CAP, BS 1364, LONGERONS 4R AND 8R. REPAIRED THE FRAME CAP IAW ER/A 570991-14, REV ORIGINAL, AND ETI-90-18-047, REV 1.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 53,648 hrs · 28,336 cycles

CRACKED WEB SURROUNDING JACKSCREW ASSEMBLY, RT SIDE AT THE VERTICAL STABILIZER. THE WEB WAS REPAIRED IAW ER/A 570884-14, REV ORIGINAL, AND ETI-90-18-043, REV 1.

Part: FRAME ANGLE — CRACKED (BS 1494) · airframe 53,648 hrs · 28,336 cycles

CRACKS ON AFT. ACC. COMP. FRAME CLIPS STA Y=1494 BTW LONGS. 2L AND 2R. AFT. ACC. COMP. FRAME CLIPS STA Y=1494 BTW LONGS. 2L AND 2R WERE REPLACED PER DWG 9953016 REV. AU AND MD90 VOL. II SRM 51-30-05 TOOL USED P/N: TEC6A S/N: 5233 D/D 26/OCT/18. (LP# 0709711)

Part: INTERCOSTAL — CORRODED (BS 826-845) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION ON INTERCOSTAL LONG 28RH BTW STA 845 TO 826 AT CENTER CARGO COMPARTMENT AMDS 5330-2616 MRB 53-302-07. LEVEL COROSION 2. INTERCOSTAL LONG 28RH BTW STA 845 TO 826 AT CENTER CARGO COMPARTMENT WAS REPLACED PER MD90 SRM VOL. II 51-30-05, MD90 SRM VOL. III 53-20-01 AND DWG 9915554 REV. J. (LP# 0710202)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE LT WING FUEL TANK ACCESS PANEL 520CT. UPPER WING ACCESS PANEL WAS REPLACED IAW AMM 28-00-00-420-801.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE RT WING FUEL TANK ACCESS PANEL 620CT UPPER WING ACCESS DOOR 520CT. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00-420-801, AND VERIFIED.

Part: FRAME ANGLE — CORRODED (BS 1344) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION ON FRAME ANGLE BS 1344 BETWEEN LONGERONS 28L AND 25R IN THE AFT CARGO. THE FRAME ANGLE WAS REPLACED IAW SRM 53-10-03, FIG 1, VOL 2, AND SRM 51-30-02, VOL 2.

Part: SKIN — DENTED (BS 1288-1307) · airframe 53,648 hrs · 28,336 cycles

FUSELAGE SKIN DENTED BETWEEN BS 1288 - 1307, LONGERON 29L - 29R.

Part: ROD END — CORRODED (LT ELEVATOR) · airframe 53,648 hrs · 28,336 cycles

RUSTED ROD END, XE=82 ON THE LT ELEVATOR FRONT SPAR. THE ROD END WAS REPLACED IAW CMM 27-30-25.

Part: CUSP WEB — CORRODED (BS 1155-1231) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

DURING REPAIR, FOUND CORROSION ON THE RT CUSP WEB BETWEEN BS 1155 - 1231. THE CUSP WEB WAS REPLACED IAW VOL.III SRM 53-10-03 FIG.11, VOL.I SRM 53-20-02 FIG 29, VOL.I SRM 53-20-02 FIG 12, VOL.II SRM 51-30-02, AND VOL.II SRM 51-30-05.

Part: CUSP WEB — CORRODED (BS 1231-1307) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

DURING REPAIR, FOUND CORROSION ON THE RT CUSP WEB BETWEEN BS 1231 - 1307. THE CUSP WEB WAS REPLACED IAW SRM 53-10-03, FIG 11, VOL III, SRM 53-20-02, FIG 29, VOL I, SRM 53-20-02, FIG 12, VOL I, SRM 51-30-02, VOL.II, SRM 51-30-05.

Part: FRAME ANGLE — CRACKED (BS 1475) · airframe 53,648 hrs · 28,336 cycles

CRACKED AFT ACCESSORY BAY FRAME ANGLES BS 1475, LONGERONS 16L&R AND 19 R. THE FRAME ANGLES WERE REPLACED IAW SRM 51-30-05, VOL II, AND DWG S1464575, REV A.

Part: STIFFENER — CRACKED (BS 1395 BULKHEAD) · airframe 53,648 hrs · 28,336 cycles

CRACKED AFT PRESSURE BULKHEAD STIFFENER, LONGERON 1, BS 1395. THE AFT PRESSURE BULKHEAD STIFFENER WAS REPLACED IAW SRM 51-30-05, VOL.II, AND SRM 51-30-02, VOL II.

Part: CHANNEL — CRACKED (MLG DOOR FRAME) · airframe 53,648 hrs · 28,336 cycles

CRACKED CHANNEL IN THE RT MLG WHEEL WELL, FWD DOOR FRAME. THE CHANNEL WAS REPLACED IAW SRM 51-30-02, VOL II, AND SRM 51-30-05, VOL II.

Part: PAN — CRACKED (R1 DOOR) · airframe 53,648 hrs · 28,336 cycles

CRACKED INNER PAN BS 168, BEAM 4 AT FWD R1 SERVICE DOOR. THE INNER PAN WAS REPAIRED IAW SRM 52-01-01, PAR 8, FIG 9, VOL 1.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 53,648 hrs · 28,336 cycles

CRACKED INTERCOSTAL BS 185 BETWEEN BEAMS 4-5, IN THE FWD PASSENGER DOOR. THE INTERCOSTAL WAS REPLACED SRM 51-30-02, AND 51-30-05, VOL II.

Part: CUSP WEB — CORRODED (BS 693-703) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE LT CUSP WEB, BS 693 TO 703. LBL 54 AND 60. FOUND TO BE OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 11, VOL 1.

Part: CUSP WEB — CORRODED (BS 826-864) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORRODED CUSP WEB, BS 826 TO 864, LBL 44 AND 54, FOUND TO BE OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 11, VOL I.

Part: CUSP WEB — CORRODED (BS 1041-1063) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE CUSP WEB, BS 1041 - 1063, BTW X 44 AND X 54. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-02, FIG 12, VOL I.

Part: CUSP WEB — CORRODED (BS 924-943) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE CUSP WEB, BS 924 - 943, X=44 AND X=54. FOUND TO BE OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, VOL 1 .

Part: CUSP WEB — CORRODED (BS 712-731) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE RT CUSP WEB, BS 712 TO 731, X=54 AND X=60. THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 14, VOL I.

Part: WEB — CRACKED (BS 171) · airframe 53,648 hrs · 28,336 cycles

CRACKED INTERNAL WEB BS 171 IN BEAM 3 AT THE L1 DOOR. THE WEB WAS REPAIRED IAW SRM 52-00-01.

Part: LONGERON — CRACKED (BS 1364) · airframe 53,648 hrs · 28,336 cycles

CRACKED LONGERON 6L, BS 1364. THE LONGERON WAS REPAIRED SRM 53-10-01, FIG 7, VOL I.

Part: FLOOR SUPPORT — CRACKED (BS 1328-1344) · airframe 53,648 hrs · 28,336 cycles

CRACKED FLOOR SUPPORT, BS 1328 - 1344. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-05 VOL. II.

Part: SKIN — DENTED (BS 236) · airframe 53,648 hrs · 28,336 cycles

DENT FOUND ON A PREVIOUS REPAIR, BS 236 BETWEEN LONGERONS 17L & 18L IN THE FUSELAGE SKIN. THE SKIN WAS REPLACED IAW SRM 53-30-01, FIG 8B, VOL I.

Part: LONGERON — CRACKED (BS 1364) · airframe 53,648 hrs · 28,336 cycles

CRACKED LONGERON 5L, BS 1364. REPAIRED IAW SRM 53-10-01, FIG 7, VOL I.

Part: CUSP WEB — CORRODED (BS 864-880) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE CUSP WEB, BS 864 TO 880, BETWEEN X=44 AND X=54. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-20-02, FIG 9, VOL II.

Part: PAN — CRACKED (MID CARGO DOOR) · airframe 53,648 hrs · 28,336 cycles

AFTER REMOVAL OF STOP FITTING NR 4, ONE CRACK WAS FOUND ON THE PAN AT THE MID CARGO DOOR FWD EDGE. THE PAN WAS REPAIRED IAW SRM 52-30-02, FIG 2, VOL I.

Part: LONGERON — CRACKED (BS 575) · airframe 53,648 hrs · 28,336 cycles

CRACKED LONGERON 2R, BS 575. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, VOL I.

Part: SUPPORT — CRACKED (BS 69-79) · airframe 53,648 hrs · 28,336 cycles

CRACK SUPPORT ON THE LT TUNNEL BETWEEN BS 76 AND 69 WITHIN THE NLG WHEEL WELL. THE SUPPORT WAS REPLACED IAW SRM 51-30-05, VOL.

Part: PAN — CRACKED (BS 1079-1136) · airframe 53,648 hrs · 28,336 cycles

CRACKED LT RING PAN, BS 1079, 1098, 1117, AND 1136. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.

Part: PAN — CRACKED (BS 845) · airframe 53,648 hrs · 28,336 cycles

CRACKED RT RING PAN, BS 845. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.

Part: FLOOR SUPPORT — CRACKED (BS 1344-1364) · airframe 53,648 hrs · 28,336 cycles

CRACKED FLOOR SUPPORT BL 0, BTW BS 1344 & 1364. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-10-03, VOL III.

Part: PAN — CRACKED (BS 1155-1288) · airframe 53,648 hrs · 28,336 cycles

CRACKED RT RING PAN AT BS 1155, 1174, 1231, 1250, AND 1288. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.

Part: FLOOR SUPPORT — CORRODED (BS 160-198) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE FLOOR SUPPORT RBL 54, BS 160 - 198. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-02, VOL II, AND SRM 51-30-05, VOL II.

Part: CUSP WEB — CORRODED (BS 756) · corrosion level 2 · airframe 53,648 hrs · 28,336 cycles

CORROSION FOUND ON THE RT CUSP WEB, BS 756, RBL 54 - 58 . THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 18, VOL. I.

Part: CUSP WEB — CRACKED (BS 897-907) · airframe 53,648 hrs · 28,336 cycles

CRACKED RT CUSP WEB, BS 897 TO 907, RBL 54 AND 56. THE CUSP WEB WAS REPAIRED SRM 53-20-02, VOL 1.

Part: CUSP WEB — DENTED (BS 334-336) · airframe 53,648 hrs · 28,336 cycles

DENT FOUND ON THE RT CUSP WEB, BS 334 TO 336, BETWEEN LBL 51 AND 54 IN THE PAX CABIN. DAMAGED AREA WAS REPAIRED IAW SRM 53-00-01, FIG 2, VOL L.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 53,070 hrs · 28,002 cycles

OBSERVED A RIGHT HYDRAULIC SYSTEM PRESSURE LOW ON OAP. PERFORMED QRH PROCEDURE AND WAS NOT ABLE TO PRESSURIZE THE SYSTEM. USED MANUAL GEAR EXTENSION PROCEDURE. REPLACED THE RIGHT ENGINE DRIVEN PUMP. REPLACED DAMAGED LINE LOCATED AT RT THRUST REVERSER BYPASS HANDLE WITH SERVICEABLE ONE. REPLACED ENGINE SCAVENGE FILTERS. LINE AND FILTERS LEAK CHECK GOOD. RIGHT THRUST REVERSER OPERATION CHECKED GOOD.

Part: AIRSTAIR — OUT OF ADJUST (TAIL) · airframe 53,065 hrs · 27,999 cycles

TAIL STAIR CATWALK OUT OF RIG, BINDS AND CATCHES WHEN LOWERING AND WHEN RAISING. ADJUSTED TAIL STAIR CATWALK IAW AMM 53-25-01. OPS OK FOR SERVICE.

Part: ANGLE — CRACKED (BS 1503) · airframe 53,057 hrs · 27,995 cycles

BS 1503.801, ANGLE WAS FOUND CRACKED BETWEEN LONGERON 1 & 3. REMOVED AND REPLACED THE ANGLE IAW SRM 53-10-04, AND 51-30-05.

Part: SHEAR TIE — CRACKED (BS 1503) · airframe 53,057 hrs · 27,995 cycles

FOUND THE BS 1503.801, SHEAR TIE BETWEEN LONGERONS 1 & 3 RIGHT CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9911840.

Part: SHEAR TIE — CRACKED (BS 1503) · airframe 53,057 hrs · 27,995 cycles

BS 1503.801 SHEAR TIE BETWEEN LONGERONS 1 & 3 WAS FOUND CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9911840, SRM 53-10-04, AND 51-30-05 JOB.

Part: SHEAR TIE — CRACKED (BS 1488) · airframe 53,057 hrs · 27,995 cycles

FOUND THE BS 1488.009 SHEAR TIE BETWEEN LONGERONS 2L & 3L CRACKED. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CRACKED (BS 1473) · airframe 53,057 hrs · 27,995 cycles

BS 1473.107. SHEAR TIE AT LONGERONS 2L & 2R CRACKED. REMOVED THE SHEAR TIE. MANUFACTURED A NEW SHEAR TIE IAW SRM 52-10-04. INSTALLED IAW SRM 53-10-04, AND 51-30-05.

Part: RELAY — FAILED (POWER TRANSFER) · airframe 52,910 hrs · 27,907 cycles

DURING TAKE OFF, ENGAGED AUTO-THROTTLES AT 70 KNOTS. DC BUSS OFF MESSAGE APPEARED ON THE EPCU ANNUNCIATOR PANEL. ALL OTHER SYSTEMS & INDICATIONS NORMAL BEFORE AND AFTER ATO. PERFORMED NO GO ODI PREVENTION CHECK LIST. FOUND DC EMERGENCY POWER TRANSFER RELAY R2-326 FAILED. REPLACED THE RELAY. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,006 hrs · 27,379 cycles

EMERGENCY CEILING LIGHTS AT ROW 35 AND 37 3 TOTAL INOPERATIVE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY IAW MM. OPERATION CHECKS GOOD.

Part: CABLE — BROKEN · airframe 51,707 hrs · 27,180 cycles

LEFT CATWALK CABLE IS BROKEN. REPLACED CABLE TURN BARREL CLEVIS CHECKED OK.

Part: OIL SYSTEM — LEAKING (RT ENGINE) · airframe 51,246 hrs · 26,906 cycles

DIVERTED DUE TO RT ENGINE OIL QUANTITY WENT TO ZERO AND OIL PRESSURE BELOW 60 PSI. FOLLOWED QRH IFSD OF RIGHT ENGINE. MAINTENANCE FOUND RIGHT ACOC LEAKING OIL. REMOVED AND REPLACED ACOC IAW MM. FUNCTIONAL CHECKED GOOD, NO CONTAMINATION. SERVICED. AIRCRAFT OKAY FOR SERVICE.

Part: GROUND WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 50,931 hrs · 26,737 cycles

CAT WALK EMERGENCY LIGHT INOPERATIVE. FOUND GROUND WIRE ON WRONG STUD. MOVED WIRE TO CORRECT STUD. OPERATION CHECKED GOOD.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 50,599 hrs · 26,567 cycles

FUMES /SMOKE IN REAR OF AIRCRAFT AFTER APU START. DISSIPATED AFTER ENGINE START AND APU SHUTDOWN. APU REPLACED AND DUCT BURNOUT PERFORMED.

Part: FUEL CONTROL — LEAKING (APU) · airframe 50,599 hrs · 26,567 cycles

SMOKE AND FUMES FROM TAIL OF AIRCRAFT AFTER APU START. MAINTENANCE TROUBLESHOT AND FOUND FUEL LEAKING FROM THE FILTER BOWL AND STUDS IN FUEL CONTROL UNIT BENT. REMOVED AND REPLACED FUEL CONTROL PER MM. OPERATION CHECKS GOOD.

Part: LOCK — WORN (TAILCONE RELEASE) · airframe 50,548 hrs · 26,539 cycles

TAIL CONE RELEASE MECHANISM UPPER LOCK FOUND WORN. REMOVED AND REPLACED UPPER LEFT LOCK PIN ASSEMBLY IAW TASK 53-52-01-211-802.

Part: FUEL CONTROL — LOOSE (APU) · airframe 50,429 hrs · 26,469 cycles

FUME, FLIGHT CREW REPORTS A FUEL SMELL IN CABIN AS THE APU WAS STARTED. PASSENGERS DEPLANED. MAINTENANCE FOUND APU FCU FILTER BOWL LOOSE AND LEAKING. RESECURED FILTER. PERFORMED DUCT BURNOUT. NO FURTHER ODOR PRESENT.

Part: STRUCTURE — DENTED (L1 DOOR) · airframe 50,153 hrs · 26,318 cycles

DENT ON LOWER LEFT EDGE FLANGE OF L1 DOOR. REPAIRED IAW SRM 52-01-01.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,007 hrs · 26,247 cycles

WING CENTER SECTION UPPER SKIN IS CORRODED, STA 943 - 962, LBL 57. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 5538514AD.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 50,007 hrs · 26,247 cycles

LONGERON 2L CRACKED AT STA 1475. REPAIRED IAW ERA 55358-14, REV O.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

MULTIPLE CORROSION SPOTS FROM STA 180-200 LBL7. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 553855-14, REV O.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

LONGERON 2R IS CRACKED, STA 1475, FUSELAGE SKIN. REPAIRED IAW SRM 53-30-01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

FOUND RADIO ALTIMETER ANTENNA DOUBLER BROKEN DUE TO CORROSION, STA 693, L30 - L29L. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-02 AND DWG 5911412.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

UPON REMOVAL OF RADIO ALTIMETER ANTENNA, LANDING DOUBLER FOR ANTENNA FOUND TO BE CORRODED BETWEEN STA 769-788, L29L. COMPLIED WITH ERA 553857-14, REV O.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

MAIN CABIN FORWARD WET AREA FLOOR SUPPORT, STA 200, LBL 10 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

MAIN CABIN FLOOR SUPPORT, STA 200, BL0 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-30-05 AND DWG 9936535.

Part: FLOOR SUPPORT — CORRODED (BS 180) · airframe 49,984 hrs · 26,232 cycles

MAIN CABIN FORWARD WET AREA FLOOR SUPPORT, BS 180, RBL 41 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 9936534.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

SEAT TRACK CORRODED, STA 200-237, LBL 44. CROWN AND BASE. FOUND OUT OF LIMITS. REPAIRED SEAT TRACK SECTION, STA 200-268, LBL 44 IAW SRM 53-40-01.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 49,984 hrs · 26,232 cycles

MAIN CABIN FORWARD WET AREA MEMBRANE, STA 201, LBL 7 IS CORRODED. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-00-01.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 49,582 hrs · 26,030 cycles

L1 DOOR SLIDE HAS RIG PIN AND LACING UNSECURED. REMOVED AND REPLACED L1 SLIDE IAW AMDS 2561-4641.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,039 hrs · 25,689 cycles

F/A REPORTED STRONG ELECTRICAL BURNING ODOR OVER SEAT 2B. CREW TURNED OFF OVERHEAD LIGHTS, GALLEY LIGHTS AND POWER AT DOOR 1L. ODOR DISSIPATED. MAINTENANCE TROUBLESHOT. NO ODOR NOTICED. UNABLE TO DUPLICATE. PERFORMED PACK BURNOUT. CHANGED COALESER BAGS.

Part: DEPRESSOR — CRACKED (ACCESS PANEL) · airframe 48,683 hrs · 25,474 cycles

PRESSURE BULKHEAD ACCESS PANEL 115AZ SEAL DEPRESSOR CRACKED. REPAIRED IAW ERA 548990-14, REV O.

Part: LANYARD — FRAYED (L2 DOOR SLIDE) · airframe 48,683 hrs · 25,474 cycles

L2 DOOR SLIDE LANYARD FRAYED. REPLACED IAW MM.

Part: SKIN — CRACKED (BS 1437) · airframe 48,651 hrs · 25,455 cycles

AIRCRAFT SKIN HAS 3 SMALL CRACKS NEAR BS 1437, L13L. COMPLIED WITH PRI/ERA 548968-14. REV O.

Part: SKIN — CRACKED (BS 1437) · airframe 48,651 hrs · 25,455 cycles

LEFT AFT SKIN BS 1437, L13L IS CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · airframe 48,651 hrs · 25,455 cycles

CORROSION ON FLOOR SUPPORT AT BS 180-200. REPLACED THE FLOOR SUPPORT IAW DWG 9936534.

Part: WEB — CORRODED (BS 200) · airframe 48,651 hrs · 25,455 cycles

CORROSION ON FLOOR WEB AT BS 200. REPAIRED IAW SRM 51-11-01.

Part: WEB — CORRODED (BS 200) · airframe 48,651 hrs · 25,455 cycles

CORROSION ON FLOOR WEB AT BS 200. REPAIRED IAW SRM 51-11-01.

Part: FLOOR SUPPORT — CORRODED (BS 201) · airframe 48,651 hrs · 25,455 cycles

CORROSION ON FLOOR SUPPORT AT BS 201. REPAIRED IAW DWG 9936534 AND SRM 53-00-01.

Part: BRAKE — LOCKED (NR 1) · airframe 47,410 hrs · 24,743 cycles

EXPERIENCED THE NR 1 BRAKE LOCKING UP DURING TAXI OUT TO THE RUNWAY. ACFT RETURNED TO BLOCKS. MAINTENANCE FOUND THE NR 1 BRAKE ASSY AND BEARING DAMAGE. REPLACED NR 1 BRAKE ASSEMBLY AND NR 1 TIRE ASSY. INSPECTED AXLE WITH NO DAMAGE FOUND.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,751 hrs · 23,764 cycles

EMERGENCY ESCAPE LIGHTING FOR CAT WALK FOUND INOPERATIVE. R & R THE BATTERY PACK IAW WDM. OPS CHECKED OK.

Part: FAN — FAILED · airframe 45,232 hrs · 23,462 cycles

SLIGHT BURNING PLASTIC ODOR DURING CLIMBOUT. REPORTED COMING FROM VENTS IN FORWARD GALLEY. SMELLED AGAIN ON APPROACH. FOUND SMOKE DETECTOR FAN CIRCUIT BREAKER OUT IN COCKPIT. REMOVED FIRST CLASS SHROUD. FOUND FAN NOT TURNING AND EXTREMELY HOT. R & R M1-83, FIRST CLASS SMOKE DETECTOR FAN MOTOR SYSTEM TEST. CHECKS GOOD IAW AMM.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 43,334 hrs · 22,253 cycles

LT TAILCONE RELEASE CABLE FRAYED. R & R LT TAILCONE RELEASE CABLE IAW AMM. OPS CHECKS GOOD.

Part: DOOR FRAME — CRACKED (BS 924) · airframe 43,334 hrs · 22,253 cycles

FUSELAGE RT SIDE OVERWING FRAME, BS 924 RT CRACKED AT UPPER RADIUS OF FRAME TAB. R & R FRAME IAW PRI 528041-14AD.

Part: RELEASE CABLE — MISINSTALLED (TAILCONE) · airframe 43,418 hrs · 22,305 cycles

TAIL CONE RELEASE CABLES, INCORRECTLY SAFETIED AT TRIANGLE PLATE AT CANTED BS 1567. SAFETIED CABLES IAW AMM.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 42,104 hrs · 21,462 cycles

DURING SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS, AFT OF EMERGENCY HATCHES, INOPERATIVE. FOUND BATTERY PACK DISCONNECTED. RECONNECTED. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,840 hrs · 21,325 cycles

TWO CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMPS. OPS CHECKED GOOD.

Part: BULB — CONTAMINATED (WORK LIGHT) · airframe 40,554 hrs · 20,550 cycles

F/A REPORTED PLASTIC BURNING ODOR ON FINAL IN FORWARD RT GALLEY. MX FOUND WIRE TAG MELTED TO WORK LIGHT BULB IN RT GALLEY. REPLACED CEILING LIGHT. OPS CHECKED GOOD. NO ODOR NOTED.

Part: FRAME — CRACKED (RT MLG WW) · airframe 38,266 hrs · 19,258 cycles

FOUND POSSIBLE CRACK AT FORWARD FRAME OF RIGHT MAIN LANDING GEAR WHEEL WELL OPENING. MAINTENANCE REMOVED AND REPLACED FRAME PER DAL DRAWING 5930584.

Part: FRAME — CORRODED (BS 1328) · airframe 38,264 hrs · 19,256 cycles

C3 FRAME AT BS 1328 L28L-29R CORRODED. REPAIRED PER SRM 53-10-02 FIG 2 VOL 1.

Part: SEAT TRACK — GOUGED (BS 745-826) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN SEAT TRACK LT INBD BS 745-826 HAS GOUGED AT LUGS. REPAIRED PER SRM 53-40-01 FIG 6 VOL 1.

Part: FRAME — CORRODED (BS 1307) · airframe 38,264 hrs · 19,256 cycles

AFT CARGO BAY FRAME BS 1307 CORRODED FWD AND AFT SIDES. REPAIRED PER 53-10-02 FIG 2 VOL 1.

Part: SEAT TRACK — GOUGED (BS 200-313) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN BS 237 RT OTBD SEAT TRACK HEAVY CORROSION REPAIRED PER SRM VOL 1 53-40-01 FIG 6.

Part: BEAM — CORRODED (FUSELAGE) · airframe 38,264 hrs · 19,256 cycles

AFT CARGO COMPARTMENT CUTOUT LOWER HEADER BEAM IS CORRODED AND REPLACED AS PER SRM 51-30-02, 51-30-05 VOL 2 AND DWG 5930483.

Part: LONGERON — CORRODED (BS 1297) · airframe 38,264 hrs · 19,256 cycles

LONGERON 30 AT BS 1297 IS CORRODED AND REPAIRED PER SRM 53-10-03 FIG 7 VOL 1.

Part: FRAME — CORRODED (BS 1212 L29L/R) · airframe 38,264 hrs · 19,256 cycles

CARGO BAY FRAME BS 1212 L29 R/L CORRODED. REPLACED PER SRM 51-10-05 AND 51-30-02 FIG 1 AND 51-30-05.

Part: CARGO TRACK — CORRODED (BS 522-636) · airframe 38,264 hrs · 19,256 cycles

C2 CARGO TRACK AT BS 522-636 CORRODED. REPLACED PER SRM 53-40-01 FIG 7 VOL 1 AND 53-20-01 FIG 19 VOL 3 AND 51-30-01 FIG 1 VOL 1.

Part: PAN — CORRODED (DOOR FRAME) · airframe 38,264 hrs · 19,256 cycles

C1 CARGO DOOR FRAME OUTBOARD SIDE IS CORRODED AT BS 362.5-434.5 AND PAN. REPLACED PER SRM 53-60-02 FIG 11 VOL 1.

Part: DOUBLER — CRACKED (LT WING) · airframe 38,264 hrs · 19,256 cycles

LEFT WING INTERIOR XRS 146 INTERIOR SPLICE DOUBLER HAS APPROX 2.5 INCH CRACK. REPAIRED PER SRM 51-30-02 FIG 1 51-30-05 FIG 12 51-10-05 FIG 1.

Part: SEAT TRACK — CORRODED (BS 237) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN BS 237 RT OUTBOARD SEAT TRACK CORRODED. REPAIRED PER SRM 53-40-01 FIG 6 VOL 1.

Part: CARGO TRACK — CORRODED (BS 1060-1307) · airframe 38,264 hrs · 19,256 cycles

C3 CARGO LT CARGO TRACK BETWEEN BS 1060 - 1307 IS CORRODED AND REPLACED PER SRM 53-40-01 FIG 7 VOL 1 AND 53-20-01 FIG 23 VOL 3 AND 51-30-05 FIG 12 AND 51-30-02 FIG 1 VOL 2.

Part: SEAT TRACK — CHIPPED (BS 218 LBL 44) · airframe 38,264 hrs · 19,256 cycles

BS 218 LBL 44 SEAT TRACK CHIPPED. REPAIRED PER SRM 53-40-01 FIG 6 VOL 1.

Part: FRAME — CORRODED (BS 1288 L29L-R) · airframe 38,264 hrs · 19,256 cycles

C3 FRAME AT BS 1288 L29 L-R CORRODED. REPAIRED PER SRM 53-10-02 FIG 2 VOL 1.

Part: CARGO TRACK — DIRTY (BS 522-647) · airframe 38,264 hrs · 19,256 cycles

MID CARGO BAY CARGO TRACK AT LBL 28 BETWEEN BS 522 - 647 DIRTY. CLEANED PER SRM 53-40-01 FIG 7 VOL 1.

Part: CARGO TRACK — GOUGED (BS 218-522) · airframe 38,264 hrs · 19,256 cycles

CARGO TRACK AT BS 218-522 IS GOUGED AND REPAIRED PER SRM 53-40-01 FIG 7 VOL 1.

Part: CARGO TRACK — GOUGED (BS 427-527) · airframe 38,264 hrs · 19,256 cycles

C1 CARGO TRACK FROM BS 427-527 IS GOUGED AND CORRODED. REPLACED PER SRM 53-40-01 FIG 7.

Part: SEAT TRACK — GOUGED (BS 236-240) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN LT INBOARD SEAT TRACK BS 236-240 GOUGED AT LUGS. REPAIRED PER SRM VOL1 53-40-01 FIG 6.

Part: SEAT TRACK — CORRODED (BS 1227) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN LT INBD SEAT TRACK STA 1227 CORRODED. REPAIRED PER SRM 53-40-01 FIG 6 VOL 1.

Part: SEAT TRACK — GOUGED (BS 313-332) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN BS 313-332 RT OTBD SEAT TRACK GOUGED AND SCRATCHED AT LUGS. REPAIRED PER SRM 53-40-01 FIG 6 VOL 1.

Part: SKIN — DAMAGED (BS 255 L17-18L) · airframe 38,264 hrs · 19,256 cycles

LEFT SIDE OF FUSELAGE SKIN CREASED AT FRAME BS 225 BETWEEN L17 AND 18 LEFT. REPAIRED PER SRM 53-30-01 FIG 8C VOL 1.

Part: SEAT TRACK — GOUGED (BS 200-322) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN BS 200 T0 313+9 RBL 44 SEAT TRACK HAS CORROSION. REPAIRED PER SRM VOL 1 53-40-01 FIG 6 VOL2.

Part: LONGERON — CRACKED (BS 1051 L20L) · airframe 38,264 hrs · 19,256 cycles

LONGERON 20 LT IS CRACKED AT BS 1051. REPAIRED PER SRM 53-10-01 FIG 9 VOL 1.

Part: SEAT TRACK — CORRODED (BS 200-260) · airframe 38,264 hrs · 19,256 cycles

MAIN CABIN SEAT TRACK CORRODED AT LUGS. REPAIRED PER SRM 53-40-01 FIG 6 VOL 1 AND DWG ACA7414.

Part: SEAT TRACK — GOUGED (BS 1250-1270) · airframe 38,264 hrs · 19,256 cycles

SEAT TRACK AT BS 1250-1270 SCRATCHED AND GOUGED. REPLACED PER SUM 53-40-01 FIG 6 VOL 1.

Part: FRAME — CORRODED (BS 1364 L29L/R) · airframe 38,264 hrs · 19,256 cycles

FRAME BS 1364 L29L/R CORRODED AND REPAIRED PER SRM 53-10-02 FIG 2 AND DWG.