N912DE

Part: TACH GENERATOR — LEAKING (NR 1 ENGINE) · airframe 65,373 hrs · 51,248 cycles

DIRTY SOCK SMELL IN COCKPIT DESCENDING BETWEEN 17,000 AND 13,000. FAS DID NOT SMELL IT IN THE CABIN. C/W NO GO ODI PREV 2172 PER AMDS 2120-2367. FOUND NBR 1 ENG. TACH GEN. LEAKING, REF LOGS 6017312 & 6017313. C/W AMDS 2120-2368, OIL CONT. CLEANING, C/W AMDS 7100-2619 PNEU. SYS. DUCT BURNOUT. (LP6017308)

Part: DOUBLER — DAMAGED (VERTICAL STAB) · airframe 64,830 hrs · 50,746 cycles

AWR: HIDDEN ELONGATED HOLES: DURING MTC WORKS IN REF NRC S/N 00194. ELONGATED HOLE ON EXTERNAL REPAIR DOUBLER AT VERTICAL STABILIZER FIXED L/E BELOW THE SPLICE AT STATION ZFS= 52.267 WERE FOUND. EXTERNAL REPAIR DOUBLER AT VERTICAL STABILIZER FIXED L/E WAS REPLACED PER SRM 51-30-01, 51-30-05 AND ERA 469193-14 REV: A PERMANENT REPAIR. (LP1090327)

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 64,830 hrs · 50,746 cycles

AWR: HIDDEN CRACK: DURING MTC WORKS IN REF NRC S/N 00194, CRACK ON INTERNAL FINGERS DOUBLER AT VERTICAL STABILIZER FIXED L/E BELOW THE SPLICE STATION ZFS= 52.267. INTERNAL FINGERS DOUBLER AT VERTICAL STABILIZER FIXED L/E WAS REPLACED PER SRM 51-30-01, 51-30-05 AND ERA 469193-14 REV: A PERMANENT REPAIR. (LP1090319)

Part: UNKNOWN — UNKNOWN (SEAT 10C) · airframe 64,762 hrs · 50,681 cycles

PAX AT SEAT 10C WAS SHOCKED BY ELECTRICAL CONNECTION IN SEAT WHILE PLUGGING IN. UNABLE TO DUPLICATE. PASSENGER HAS LAPTOP PLUGGED IN AND STATES GETTING SHOCKED IN ARMREST. FWD TO NEF 24-58-02. DEFERRAL REMARKS C/W. INSP PED OUTLET AT 10C. ALL HARNESS SECURED AT ISPS. ALL WIRE CK GOOD. REPLACED OUTLET AS A PRECAUTION.

Part: SWITCH — OUT OF POSITION (COCKPIT) · airframe 64,411 hrs · 50,369 cycles

ELECTRICAL SHORT ABOVE CAPTAINS INSTRUMENT PANEL. REPOSITIONED LT WING LANDING LIGHT SWITCH. OP'S NORMAL. (LP5824408)

Part: TRANSFORMER — INOPERATIVE (LIGHT) · airframe 64,301 hrs · 50,280 cycles

WHILE T/S WING NACELLE & FLOOD LIGHTS C/B POPPING NOTICED ELECTRICAL SMELL AND SMOKE FILLING UP THE FIRST CLASS SECTION MAINLY. NO SMOKE IN THE AFT CABIN NOR IN THE FLIGHT DECK. NO PASSENGERS WERE ON BOARD. FOUND T1-10 TRANSFORMER INOP. R&R OF T1-10 TRANSFORMER PER AMM 33-41-02. OPS CHK NRML. ALSO R&R OF NACELLE & FLOOD LAMP. THERE WAS NOT AN NO-GO-ODI-PREVENTION EVENT AT THIS TIME. A/C OK FOR SVC.

Part: UNKNOWN — MALFUNCTIONED (AUTOTROTTLE SYS) · airframe 64,094 hrs · 50,098 cycles

THROTTLES BURST INTO ATL ON RT ENGINE. PERFORMED DFGC FLIGHT FAULT REVIEW AND FOUND NO FAULTS DISPLAYED LAST 20 LEGS. PERFORMED DFGC RTS PER AMM 22-01, BOTH GO. PERFORMED A/T CHECK OUT PER AMM 22-31, OPS CHK GOOD. SDR REPORTED DUE TO UN-COMMANDED ENGINE ACCELERATION WHILE AUTO-THROTTLES WERE ENGAGED. . (LP5280542)

Part: SLIDE — DETACHED (L1 DOOR) · airframe 63,938 hrs · 49,980 cycles

1L SLIDE PACK DETATCHED FROM CABIN DOOR WHEN CLOSING. FOUND L1 SLIDE LOWER PIN PULLED. REMOVED AND REPLACED L1 SLIDE. (LP4807772)

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,608 hrs · 49,686 cycles

CEILING EMERGENCY LIGHTS OUT ROWS 17-19 AND 27-29. REPLACED BATTERIES FOR EMERG LIGHTS AT ROWS 17-19 AND 27-29 IAW AMM 33-53. ALL EMERGENCY LIGHTS NOW CK GOOD. (LP5002976)

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 62,320 hrs · 48,575 cycles

FA REPORTED A FAINT BURNING RUBBER ODOR WHILE REACHING CRUISE ALTITUDE. COCKPIT ODOR SMELLED LIKE AN OILY ODOR. ENG ANTI-ICE WAS ON, WHEN ENGINE ANTI-ICE WAS TURNED OFF, THE ODOR SEEMED DISSIPATE. INSPECTED THE INTAKE AND BLEED AIR MANIFOLDS, BOTH ENGINES. NO CONTAMINATION FOUND. INSPECTED BELLY AND APU AREA, NO CONTAMINATION FOUND. INSPECTED THE TAIL COMPARTMENT, AND ACMS, ALL CHECKED OK. TROUBLESHOT IAW W/C 2120-2367 AND W/C 7100-2619. REMOVED AND INSPECTED CROSSFEED DUCT. PRIMARY HEAT EXCHANGER INLET ON THE LT AND RT PACKS, APU OUTLET DUCT, NO CONTAMINATION FOUND. REINSTALLED DUCTS. REMOVED AND REPLACED LT AND RT WATER COALESCE ASSYS. A/C HAD STRONG SOAP SMELL WITH PACKS ON ARRIVAL INTO ATL. NO HYD LEAKS ONR FLUID EVIDENCE ON A/C REF LOG 0516800. C/W W/C 2120-2367 WITH NO ODOR OTHER THAN SOAP. C/W W/C 7100-2619. 4CYCLES IN TOTAL OF FCV LT AND RT C/W. RAN TAKEOFF POWER AND MAX CRUISE NO FURTHER SOAP ODOR.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 61,849 hrs · 48,197 cycles

CENTER LIGHT IN AFT STAIRWELL, THE CONNECTOR FOUND BROKEN ON CEILING WHEN CATWALK IS DOWN. REPAIRED THE CONNECTOR IAW SWPM 20-30-12. EMERGENCY LIGHT OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 1474) · airframe 59,781 hrs · 46,595 cycles

AFT ACCESSORY COMPARTMENT HAD A CRACKED FRAME BS 1474 LONGERON 19L. THE FRAME WAS REPAIRED IAW ETI-88-17-101, REV 3, AND ERA 556340-14, REV ORIGINAL.

Part: FASTENER — MISSING (VERTICAL STAB) · airframe 59,781 hrs · 46,595 cycles

LOOSE AND MISSING FASTENERS ON VERTICAL STABILIZER LEADING EDGE AT THE SPLICE STA ZFS= 52. ASTENERS WERE REPLACED PER MD-88 AMM 20-30-01. REPAIR IS WITHIN LIMITS IAW SRM 55-03 FIG 30. (LP2978352)

Part: HINGE — DAMAGED (FWD CARGO DOOR) · airframe 59,781 hrs · 46,595 cycles

FWD CARGO DOOR HAS LONGATED FWD HINGE HOLE. THE HINGE WAS REPAIRED IAW ER/A 10-524489-14.

Part: SKIN — CRACKED (BS 1403) · airframe 59,781 hrs · 46,595 cycles

CRACK OF 0.195" LENGTH, WAS FOUND ON FUSELAGE SKIN AT BS 1403, LONGERON 2L. THE SKIN WAS REPAIRED IAW ERA 556329-14A0D, REV ORIG, AND ETI-88-17-088, REV 5.

Part: VANE — DELAMINATED (TE FLAP) · airframe 59,781 hrs · 46,595 cycles

DELAMINATED INTERNAL DOUBLER ON THE OTBD FLAP INBD GUIDE VANE. THE GUIDE VANE WAS REPLACED IAW SRM 57-03D, PAR 11.

Part: SUPPORT FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE LT MLG SUPPORT FITTING BUSHING BORE. REPAIRED THE SUPPORT FITTING IAW ETI-88-17-170, REV 1, AND ERA 491033-14AD, REV A.

Part: SKIN — CRACKED (BS 120-133) · airframe 59,781 hrs · 46,595 cycles

CRACKED PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN HOLD OPEN HOOK HOUSING OF L1 DOOR BS 120 - 133, LONG 14 - 16L. REPAIRED IAW ETI-88-17-105, REV 1, AND ERA 556364-14, REV ORIG.

Part: BEARING — CORRODED (RT MLG) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON BEARING OF RETRACT SUPPORT FITTING ON THE RT MLG. THE BEARING WAS REMOVE IAW CMM 20-10-7, WORKED IAW DWG SR09570087 REV. B. A NEW BEARING WAS INSTALLED IAW SOPM 20-10-7.

Part: INTERCOSTAL — CRACKED (BS 937-941) · airframe 59,781 hrs · 46,595 cycles

CRACKED LOWER INTERCOSTAL BS 937 - 941 AND RBL 60. THE INTERCOSTAL WAS REPAIRED IAW ER/A 556390-14, REV ORIGINAL, AND ETI-88-17-102, REV 3.

Part: SKIN — SCRATCHED · airframe 59,781 hrs · 46,595 cycles

SCRATCHES ON WINDOW BELT AT FWD RH EMERGENCY EXIT DOOR. WINDOW BELT AT FWD RH EMERGENCY EXIT DOOR WAS REPAIRED IAW ETI-88-17-126, REV ORIG. AND ERA 556388-14 REV ORIG.

Part: PIN — MIGRATED (FUEL DOOR) · airframe 59,781 hrs · 46,595 cycles

WEAR DAMAGE DUE TO PIN MIGRATION ON THE I/B SIDE OF THE FUEL DOOR CUTOUT ON THE RT WING IN REF LOG 1319130. THE I/B SIDE OF THE FUEL DOOR CUTOUT ON THE RT WING WAS REPAIRED PER ETI-88-17-083 REV 2 AND ERA 523305-14 REV B SECTION III AND JOB 125 UNDER LOG 1319130.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,595 cycles

AFT ACCESSORY COMPARTMENT CRACKED INTERCOSTAL STA Y=1480 CANTED BULKHEAD APPROX IN LONG PROJECTION 19L. INTERCOSTAL WAS REPLACED PER SRM 51-30-2 AND 51-30-5 AND DWG 9911946 REV R.

Part: CONTROL TUBE — CORRODED (ELEVATOR) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE LT & RT ELEVATOR CONTROL TUBES.

Part: FRAME — CRACKED (BS 1510) · airframe 59,781 hrs · 46,595 cycles

CRACKED FRAME BS 1510. REPAIRED THE FRAME IAW ER/A 497316-14MA, REV ORIGINAL.

Part: DOOR FRAME — DAMAGED (BS 194-200) · airframe 59,781 hrs · 46,595 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON A DOUBLER REPAIR AT BS 194 TO 200 OF THE LOWER AFTER DOOR FRAME AT THE FWD SERVICE DOOR. REPAIRED IAW ER/A 333312-14, REV. B.

Part: SKIN — CRACKED (RT WING) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CRACKED RT LOWER ACCESS DOOR CUTOUT BETWEEN XRS 189 AND 214, STRINGERS 12 AND 15R. REPAIRED IAW ETI-88-17-098, REV ORIGINAL, AND ERA 556348-14AD, REV ORIGINAL.

Part: BEAM — CORRODED (BS 636-670) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

MID CARGO COMPARTMENT HAD CORROSION ON PREVIUS REPAIR SPACER BS 636 - 670 ON THE CARGO DOOR FRAME LOWER BEAM. THE DOOR FRAME LOWER BEAM WAS REPAIR IAW SRM 53-05, FIG 123.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON TIE TRACK FROM STA Y=1007 TO Y=1220 LT SIDE. TIE TRACK FROM STA Y=1007 TO Y=1220 LT SIDE WAS INSTALLED PER SRM 51-30-2, SRM 51-30-5, SRM 51-30-1.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON TIE TRACK AND SPLICE FROM STA Y=1220 TO Y=1309 LT SIDE. TIE TRACK FROM STA Y=1220 TO Y=1309 LT SIDE WAS REPLACED PER SRM 51-30-2, SRM 51-30-5, SRM 51-30-1. TIE TRACK SPLICE WAS ACCOMPLISHED WITH NRC.

Part: ANGLE — CRACKED (BS 1380 FRAME) · airframe 59,781 hrs · 46,595 cycles

AFT ACCESSORY COMPARTMENT HAD A CRACKED FRAME ANGLE BS 1380 BETWEEN LONGERONS 13 AND 14R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912246, REV DE, SRM 51-30-5, AND 51-30-2. (LP2965334)

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

AFT CARGO COMPARTMENT; CORROSION ON TIE TRACK AND FROM STA Y=1007 TO Y=1155 RT SIDE. TIE TRACK AND FROM STA Y=1007 TO Y=1155 RT SIDE WAS REPLACED PER SRM 51-30-2, SRM 51-30-5, SRM 51-30-1.

Part: PAN — CRACKED (CARGO DOOR) · airframe 59,781 hrs · 46,595 cycles

CRACKED AFT OUTER PAN BETWEEN BEAMS 1 AND 2, IN THE AFT CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, FIG 26B, SHEET 2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

AFT CARGO COMPARTMENT; CORROSION ON TIE TRACK AND FROM STA Y= 1212 TO Y=1309 RT SIDE. TIE TRACK AND FROM STA Y=1212 TO Y=1309 RT SIDE WAS REPLACED PER SRM 51-30-2, SRM 51-30-5, SRM 51-30-1.

Part: FRAME — CRACKED (BS 1485) · airframe 59,781 hrs · 46,595 cycles

AFT ACCESSORY COMPARTMENT HAD A CRACKED FRAME BS 1485, BELOW VENTRAL STAIRWAY ACTUATOR. THE FRAME WAS REPAIRED IAW SRM 53-03D, FIG 43, SHEET3.

Part: INTERCOSTAL — CORRODED (WALKING BRIDGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON WALKING BRIDGE INTERCOSTALS. INTERCOSTALS WERE REPLACED PER DWG 9911993 REV CJ.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 59,781 hrs · 46,595 cycles

LEFT WING TE FLAP HAD DELAMINATED SKIN, UPPER AND LOWER SURFACE AT THE OTBD FLAP MID GUIDE VANE. REPAIRED IAW SRM 57-03D, PARAGRAPH 11, FIGURE 11.

Part: BULKHEAD — CORRODED · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON FWD BULKHEAD AT WALKING BRIDGE. AREA OUT LIMITS AND WAS REPAIRED IAW SRM 53-01, FIG 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 59,781 hrs · 46,595 cycles

LEFT WING DENTED ON UPPER AND LOWER SURFACE ON THE INBD FLAP, INBD GUIDE VANE. TAP TEST INSPECTION WAS ACCOMPLISHED AND DISBONDED AREAS WERE FOUND AT THE DENTS. THE AREA WAS REPAIRED IAW SRM 57-03D, PARAGRAPH 11, FIGURE 11.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON COUNTERSINKS OF THE FUEL ACCESS PANEL NR 1307C ON THE LT WING. THE ACCCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: BULKHEAD — CORRODED · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

AFT ACCESSORY COMPARTMENT CORRODED ON FWD AND AFT BULKHEADS AT WALKING BRIDGE. FOUND OUT LIMITS. REPAIRED.

Part: VANE — WORN (LT WING TE FLAP) · airframe 59,781 hrs · 46,595 cycles

LEFT WING HAS A WORN OTBD EDGE SKIN ON THE INBD FLAP, INBD GUIDE VANE. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PARAGRAPH 11, FIGURE 11.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

AFT CARGO BAY CORRODED ON PREVIOUS FRAME REPAIR BS 1309, LONGERON 29L IN THE AFT CARGO BAY. THE REPAIR WAS REPLACED IAW SRM 53-03D, FIG 2A.

Part: VANE — DENTED (RT WING TE FLAP) · airframe 59,781 hrs · 46,595 cycles

RIGHT WING DENTED ON PREVIOUS REPAIR DOUBLERON INBD GUIDE VANE. REPAIRED IAW SRM 57-03D, PARAGRAPH 11, AND 51-70-2D.

Part: VANE — DENTED (RT WING TE FLAP) · airframe 59,781 hrs · 46,595 cycles

RIGHT WING DENTED ON PREVIOUS REPAIR DOUBLER AT INBOARD FLAP, INBOARD GUIDE VANE. REPAIRED IAW SRM 57-03D, PARAGRAPH 11, AND 51-70-2D.

Part: SKIN — WORN (CARGO DOOR) · airframe 59,781 hrs · 46,595 cycles

:WEAR LOWER INNER AND OUTER SKIN OF THE FWD CARGO DOOR. THE DAMAGE WAS REPAIRED IAW ERA 522785-14MA, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1380) · airframe 59,781 hrs · 46,595 cycles

CRACKED LONGERON 11R BS 1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION IN THE COUNTERSINKS OF THE ACCESS PANEL FOR THE RT WING. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE COUNTERSINKS AND SEATING AREAS OF THE ACCESS PANEL 1361C FOR THE LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION II.

Part: ATTACH FITTING — CORRODED (DOOR SLIDE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON FITTING TO ATTACH FWD SERVICE GALLEY SLIDE. THE FITTING WAS REPLACED IAW SRM 51-10-4.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON COUNTERSINK ON THE ACCESS PANEL 1335C FOR THE LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION II (A) 1 AND 2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON COUNTERSINK AND SEATING AREA OF THE ACCESS PANEL 1303C FOR LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, CONDITION III.

Part: BUSHING — DAMAGED (SPOILER LINK) · airframe 59,781 hrs · 46,595 cycles

DAMAGE BUSHINGS ON GROUND SPOILER LINKS. THE LINKS WERE REPLACED IAW CMM. 27-61-10.

Part: HOUSING — WORN (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

WEAR ON HOUSING AT THE L1 DOOR. THE HOUSING WAS REPLACED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 1243-1245) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON CUSP WEB LBL 44 & 60, BS 1245 - 1243. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131 A.

Part: SKIN — NOT REPORTED · airframe 59,781 hrs · 46,595 cycles

ERA491693-14AD REV B, FUSELAGE SKIN LT & RT WINDOW BELT PANEL. WINDOW BELT PANEL WAS REPLACED IAW ER/A 491693-14AD, REV C, AND DRAWING 5953608, REV C.

Part: HINGE — CRACKED (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

CRACKED HINGE ATTACH LOWER EDGE AT FWD L1 DOOR. THE HINGE WAS REPLACED IAW SRM 51-30-1, AND 51-30-4.

Part: CUSP WEB — DAMAGED (BS 464) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CUSP WEB DAMAGED BS 464, RBL 58. REPAIRED IAW SRM 53-05, FIG 131A-10.

Part: HOUSING — WORN (CARGO DOOR) · airframe 59,781 hrs · 46,595 cycles

WORN HOUSING AT MID CARGO DOOR. THE HOUSING WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

L1 DOOR HAD A CRACK ON THE INTERCOSTAL BETWEEN BEAMS 4 AND 5. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-1, AND 51-30-2.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE HORIZONTAL STAB SKIN AT THE BARREL NUTS NR 9 AND 25, XH 27. REPAIRED IAW ETI-88-17-089, REV 2, AND ER/A 556330-14, REV ORIGINAL.

Part: DOUBLER — CRACKED (DOOR PAN) · airframe 59,781 hrs · 46,595 cycles

CRACKED DOUBLER ON THE AFT PAN BETWEEN BEAM 1 AND 2 ON THE AFT CARGO DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-30-5, AND DWG 9957664, REV N.

Part: CUSP WEB — CORRODED (BS 1163-1164) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION THE ON CUSP WEB BETWEEN BS 1163 - 1164, RBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131.

Part: CUSP WEB — CORRODED (BS 1003-1022) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE CUSP WEB UPPER & LOWER SURFACE RBL 54 - 60, BS 1003 - 1022. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-4.

Part: BEAM — CRACKED (BS 1212) · airframe 59,781 hrs · 46,595 cycles

FWD CARGO BAY DOOR CRACKED INNER PAN BEAM NR 5, BS 1212. REPAIRED IAW SRM 52-03D FIG 8.

Part: CUSP WEB — CORRODED (BS 598-712) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON LEFT LOWER AND UPPER CUSP WEB SURFACE BS 598 TO 712, LBL 44 - 60. THE CUSP WEB WAS REPLACED IAW SRM 53-05 FIG 131A-24 .

Part: CUSP WEB — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE RT CUSP WEB, BS 1060 - 1079, RBL 54 - 60. THE DAMAGE AREA WAS REPAIRED SRM 53-05, FIG 131A-9.

Part: CUSP WEB — CORRODED (BS 984-1010) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE PREVIOUS REPAIR OF THE PAX CABIN CUSP WEB BS 984 TO 1010, LBL 54 TO 60. THE CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-24.

Part: SEAT TRACK — DAMAGED (BS 607-609) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

SEAT TRACK BS 607 - 609, LBL 54 DAMAGED OUT OF LIMITS. THE DAMAGE WAS REPAIRED IAW SRM 53-05, FIG. 4A.

Part: CUSP WEB — CRACKED (BS 712-715) · airframe 59,781 hrs · 46,595 cycles

CRACK ON RT CUSP WEB BETWEEN BS 712 TO 715, RLB 54 TO 60 . DAMAGE AREA WAS REPAIRED IAW SRM 53-05- FIG.131A-10.

Part: SKIN — DENTED (LT AILERON) · airframe 59,781 hrs · 46,595 cycles

DENT ON UPPER SKIN ON LT AILERON. THE AILERON WAS REPAIRED IAW SRM 51-70-1A, PAR. 12.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 59,781 hrs · 46,595 cycles

WEAR ON THE FWD AND AFT LOWER CORNERS OF THE DOUBLERS ON THE AFT CARGO DOOR. THE DOUBLERS WERE REPLACED IAW SRM 51-30-2.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 59,781 hrs · 46,595 cycles

FWD WET AREA, CORROSION AND CRACKED ANGLES ON RT FLOOR PANEL 160G. THE FLOOR PANEL WAS REPLACED IAW DWG 9957828, SRM 51-30-2, 51-10-3, PAR 26, 14, AND 21, 51-10-4, AND 51-10-2.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION OUT OF LIMITS ON RT LOWER AND UPPER CUSP WEB SURFACE BS 579 TO 582, BS 595 - 598, RBL 44 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: LONGERON — WORN (BS 1408) · airframe 59,781 hrs · 46,595 cycles

WEAR ON LONGERON 8L, BS 1408. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: SEAT TRACK — DAMAGED (BS 484-486) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

OUT OF LIMITS SEAT TRACK BS 484 - 486, LBL 54 IN THE CABIN. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 4A .

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION OUT OF LIMITS ON FLOOR PANEL 120D. A NEW FLOOR PANEL WAS DRILLED IAW SRM 51-10-4. TREATED AND PAINTED IAW SRM 51-10-3PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 579-598) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE PAX CABIN RT CUSP WEB UPPER & LOWER SURFACES BS 579 - 598, RBL 44 - 60. THE CORROSION WAS REMOVED, TREATED, AND PAINTED IAW SRM 51-10-3, PAR 26, 14, 21, AND 38. FOUND TO BE OUT LIMITS.

Part: FAIRING — DAMAGED (RT ELEVATOR) · airframe 59,781 hrs · 46,595 cycles

CRACK ON RT ELEVATOR CONTROL TAB FAIRING. TAB FAIRING WAS REPAIRED IAW SRM 55-01 FIG.2.

Part: FLOOR SUPPORT — CRACKED (BS 1309) · airframe 59,781 hrs · 46,595 cycles

AFT CARGO BAY, CRACKED FLOOR SUPPORT BS 1309 BL 0. THE FLOOR SUPPORT WAS REPLACED IAW DWG 5930560, REV BC, SRM 51-30-2, AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 59,781 hrs · 46,595 cycles

DELAMINATED FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED AMM 53-20-01-201.

Part: CUSP WEB — CORRODED (BS 1255-1266) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON CABIN FLOOR CUSP WEB UPPER/LOWER SURFACES RBL 54 - 60, BS 1255 - 1266. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131 A-7.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,595 cycles

DERIVED OF INSPECTION HFEC ON CUSP WEB WAS FOUND CRACK OF STA Y=1039 BTW X -54 TO X - 60 AT CABIN PAX. CUSP WEB WAS REPAIRED OF STA Y=1039 BTW X-54 TO X-60 PER SRM 53-05 FIG 131A-9.

Part: FAIRING — DAMAGED (LT ELEVATOR) · airframe 59,781 hrs · 46,595 cycles

PROTUBERANCE ON FAIRING BETWEEN ANTIFLOAT TAB AND GEARED TAB ON LT ELEVATOR. FAIRING WAS REPAIRED IAW SRM 55-01 FIG. 2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE X=-54 X=-60 FROM STA Y=807 TO STA Y=845. AREA OUT LIMITS BTW STA Y= 826 TO 845 WAS REPAIRED PER SRM 53-05 FIG 131A-10. AREA BTW STA Y=807 TO 826 WAS RE-INSPECTED AND NOT CORROSION WAS FOUND.

Part: STEP — CORRODED (VENTRAL STAIRS) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION AT VENTRAL STAIRWAY STEP NR 12. STEP NR 12 WAS REPLACED PER SRM 52-60-0.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 59,781 hrs · 46,595 cycles

SCRATCHES WERE FOUND AFFECTING THE LT WINDOW BELT PANEL BTW STA Y=598 - 674 IN REF TO NRC S/N 00159. SCRATCHES ON WINDOW BELT WERE REPAIRED PER ETI-88-17-084 REV ORIGINAL AND ER/A 556323-14 REV ORIGINAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE X=-54 X=-60 FROM STA Y=1079 TO STA Y=1098. CUSP WEB WAS REPLACED PER SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — DELAMINATED · airframe 59,781 hrs · 46,595 cycles

DELAMINATED ON FLOOR PANEL. FLOOR PANEL WERE FABRICATED PER AMM 53-20-01-201.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,595 cycles

AFT WET AREA, CRACK AND BEND FLOOR SUPPORT ON STA Y= 1309 TO STA= 1347 AND X= -17 AMDS 5300-2586. NEW FLOOR SUPPORT WAS REPLACED PER SRM 51-30-1 AND DWG 9936656 REV AM.

Part: DOUBLER — WORN (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

L1 DOOR HAS WEAR ON THE EXTERNAL DOUBLER, HOOK AREA. EXTERNAL DOUBLER WAS REPLACED IAW SRM 52-05, FIG 20A.

Part: CUSP WEB — CRACKED (BS 767-769) · airframe 59,781 hrs · 46,595 cycles

CRACKED LEFT CUSP WEB BETWEEN BS 767 - 769 AND LBL 50 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131, A-18.

Part: PAN — CRACKED (BS 845) · airframe 59,781 hrs · 46,595 cycles

CRACK FOUND ON RT UPPER CORNER RING PAN BS 845. RT UPPER CORNER RING PAN WAS REPAIRED IAW SRM 53-05, FIG. 122, AND ER/AS 493648-14MA.

Part: PAN — CRACKED (CARGO DOOR) · airframe 59,781 hrs · 46,595 cycles

CRACKED INNER PAN ON FWD EDGE BELLOW STOP FITTING NR 3 AT AFT CARGO DOOR. THE INNER PAN WAS REPAIRED IAW SRM 52-05, FIG 50.

Part: STEP — CORRODED (VENTRAL STAIR) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON VENTRAL STAIRWAY STEPS 1, 3, 4, 5, AND 6 SETTLEMENT AREA. STEPS 5, AND 6 WERE DRILLED AND ADJUSTED IAW SRM 52-60-0, CORROSION WAS REMOVED ON VENTRAL STAIRWAY STEPS 1, 3, & 4.

Part: MECHANISM — CORRODED (RUDDER SYSTEM) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

AFT ACCESSORY COMPARTMENT, CORROSION ON BELLCRANK AT RUDDER THROW-LIMITER MECHANISM. BELLCRANK AT RUDDER THROW-LIMITER MECHANISM WAS REPLACED AND INSTALLED PER RII AMDS 2720-2325 STEP NR 6 AND MUST BE ADJUSTED PER RII AMDS 2720-2325 STEP NR 7.

Part: FINGER DOUBLER — DEBONDED (BS 218-256) · airframe 59,781 hrs · 46,595 cycles

DEBONDED FINGER DOUBLER ON PREVIOUS REPAIR ON INTERNAL FUSELAGE SKIN BETWEEN BS 218 - 256, LONGERON 16 - 17L. THE FINGER DOUBLER WAS REPLACED IAW SRM 53-04-3, FIG.12 (SHEET2).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

FWD WET AREA: CORROSION ON FLOOR SUPPORTS BTW STA Y=148 AND Y=218 BTW X=0 AND X=-60. FLOOR SUPPORTS WERE REPLACED PER SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 845) · airframe 59,781 hrs · 46,595 cycles

CRACK ON THE FRAME AT BS 845, LONGERON 11R. THE SPLICE AND FRAME ANGLE WERE REPLACED IAW DWG 9936517, REV ORG, AND SRM 53-03 D, FIG 3.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON THE LT AND RT ANGLES AT LOWER AFT ENTRY DOOR AREA. THE ANGLES WERE REPLACED IAW SRM 51-30-4, 51-30-5, AND DWG 9915565, REV BD.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

LEFT WING TE FLAP SKIN CORRODED, UPPER AND LOWER SURFACES AT THE OTBD FLAP, OTBD GUIDE VANE. REPLACED IAW DWG 5910043 REV AU.

Part: FITTING — CRACKED (BS 1174) · airframe 59,781 hrs · 46,595 cycles

:CRACKED FITTING BS 1174 UPPER EDGE INTERNAL STRUCTURE. THE FITTING WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

AWR SECOND TIER: CORROSION ON TRACK AT WET AREA 1 BTW STA Y=148 AND Y=200 AT X=7. FLOOR SUPPORT WAS REPLACED PER SRM 51-30-1.

Part: LONGERON — CRACKED (BS 541) · airframe 59,781 hrs · 46,595 cycles

CRACK ON LONGERON 4R, BS 541 AT INTERNAL FUSELAGE STRUCTURE BEHIND LIFE RAFT SUPPORT. THE LONGERON WAS REPAIRED IAW 53-02, FIG 18.

Part: CUSP WEB — DAMAGED (BS 1022-1079) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON CUSP WEB UPPER/LOWER SURFACE RBL 54 - 60, BS 1022 - 1079. FOUND CRACKED. REPAIRED IAW ER/A 511165-14MA.

Part: SEAT TRACK — CORRODED (BS 516-518) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON SEAT TRACK LBL 22, FROM BS 516 - 518. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 4A.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 59,781 hrs · 46,595 cycles

RIGHT WING DENTED ON SKIN LOWER SURFACE AT THE INBD FLAP, OTBD GUIDE VANE. THE GUIDE VANE IAW SRM 57-03D, PAR 11 WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 218-237) · airframe 59,781 hrs · 46,595 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 218 AND 237, RBL 54 AND 60. REPAIRED IAW SRM 53-05, FIG 131A-13. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND.

Part: PAN — CRACKED (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

L1 DOOR CRACKED ON INNER PAN , THE PAN WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-4 AND 51-30-5.

Part: TAB — DENTED (LT HORIZ STAB) · airframe 59,781 hrs · 46,595 cycles

HORIZONTAL STABILIZER, DENT 1EA ON LT CONTROL TAB NEAR STA XHS= 68. LT CONTROL TAB NEAR STA XHS= 68 WAS REPAIRED PER SRM 55-04 FIGURE 2.

Part: BUSHING — CORRODED (RUUDER) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON UPPER BUSHING AT RUDDER UPPER HINGE. UPPER BUSHING ON UPPER HINGE RUDDER WAS REPLACED PER SOPM 20-10-7.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON LT LOWER AND UPPER CUSP WEB SURFACE STA Y= 863 TO Y=865 BTW X=44 TO X=60 AMDS 5300-2586. DAMAGE AREA WAS REPAIRED PER SRM 53-05 FIG 131A-1.

Part: REPAIR — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON LT PREVIOUS REPAIR CUSP WEB STA Y=1178 BTW X=54 TO X=60 AMDS 5300-2586. PREVIOUS REPAIR WAS REPLACED PER SRM 53-05 FIG 131A-6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON RT SEAT TRACK X=-22 BTW STA Y=200 AND Y=256. SEAT TRACK WAS REPLACED PER SRM 53-05 FIG 4H AND 51-30-1, 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,595 cycles

PAX CABIN, CRACK ON RT UPPER CORNER RING PAN STA Y =1003. RING PAN WAS REPAIRED PER SRM 53-05 FIG 122 AND ER/AS 493648-14MA REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,595 cycles

CRACK ON RT LWR CORNER RING PAN STA Y =1117. RING PAN WAS REPAIRED PER SRM 53-05 FIG 122 AND ER/AS 493648-14MA REV A AND 487747-14MA REV A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,595 cycles

CORROSION ON FLOOR SUPPORT ANGLES STA Y=120 AND Y=148 AT X=-44. FLOOR SUPPORT STA Y=120 AND STA Y=148 AT X=-44 WAS REPLACED PER SRM 53-14-1 FIG.11 AND 51-10-8.

Part: TAB — DAMAGED (LT HORIZ STAB) · airframe 59,781 hrs · 46,595 cycles

HORIZONTAL STABILIZER, PROTUBERANCE ON LT CONTROL TAB NEAR STA XHS= 86. LT CONTROL TAB NEAR STA XHS= 86 WAS REPAIRED PER SRM 55-04 PAR 3 CLASS A.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · airframe 59,781 hrs · 46,595 cycles

AFT CARGO BAY, CORROSION ON PREVIOUS REPAIR SPACER ON DOOR FRAME LOWER BEAM BS 1155 - 1212. THE REPAIR WAS REPLACED IAW SRM 53-05, FIG 123.

Part: DOUBLER — DAMAGED (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

BENT AND NICKED EXTERNAL DOUBLER ON BOTTOM AREA OF THE L1 DOOR. DOUBLER THE WAS REPLACED IAW SRM 52-05 FIG. 37 (SHEET 1).

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 59,781 hrs · 46,595 cycles

CRACK ON FLOORS PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 53--05, PAR 145, FIG 131B, AND 131C.

Part: SKIN — CRACKED (BS 886-1041) · airframe 59,781 hrs · 46,595 cycles

SKIN PANEL CRACKED BS 1041, 1022, 984, 946, AND BS 886. DAMAGED AREAS WERE REPAIRED IAW SRM 53-05 FIG. 122.

Part: BEAM — CRACKED (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

L1 DOOR CRACKED BEYOND STOP DRILL ON PREVIOUS REPAIR BEAM 1. THE BEAM FWD EDGE WAS REPAIRED IAW SRM 52-05 FIG. 98 (SHEET 3).

Part: SPAR — DAMAGED · airframe 59,781 hrs · 46,595 cycles

DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND SEVEN DIFFERENT FASTENERS OF PSE ON LOWER SKIN BETWEEN XRS 163 TO 168 REAR SPAR AT RT WING.

Part: BEAM — CRACKED (L1 DOOR) · airframe 59,781 hrs · 46,595 cycles

L1 DOOR. CRACK ON BEAM 1 , AFT EDGE AT MAIN ENTRANCE DOOR. BEAM 1 , AFT EDGE WAS REPAIRED IAW SRM 52-05, FIG 81, SHEET 3.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 59,781 hrs · 46,595 cycles

EMERGENCY EXIT DOOR HAS A CRACK ON ANGLE THAT ATTACH THE BEAM WITH THE INNER PAN . THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,531 hrs · 46,420 cycles

CENTER CEILING EMERGENCY LIGHTS 11-20 LEFT SIDE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS AT BS 731 AND 500 IAW AMM 33-53. OPS CHECKED GOOD.

Part: DOOR FRAME — CRACKED (MLG DOOR) · airframe 57,254 hrs · 44,703 cycles

LEFT WHEEL WELL FWD DOOR JAM CRACKED. STOP DRILLED CRACK ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR IAW ERA 544047-14. PERMANENT REPAIR TO BE ACCOMPLISHED IAW ERA 544047-14 WITHIN 10 DAYS FWD TO MON.

Part: DUCT — DISCONNECTED (CABIN AIR) · airframe 55,451 hrs · 43,404 cycles

F/A REPORTED SMOKE BUILDING IN THE AFT CABIN ON FINAL APPROACH ACCOMPANIED BY THE AFT RT LAVATORY SMOKE DETECTOR IN ALARM. VISIBLE SMOKE WAS OBSERVED INSIDE LAVATORY SO THE F/A DISCHARGED THE PORTABLE FIRE EXTINGUISHER INTO THE AFT LAVATORY AND SECURED THE DOOR. MAINTENANCE FOUND A GASPER DUCT BEHIND THE AFT LAVATORY MIRROR DISCONNECTED AND EMITTING MIST. THE DUCT WAS SECURED AND A PNEUMATIC SYS BURN-OUT WAS PERFORMED. NO FURTHER VISIBLE SMOKE AND NO ODORS NOTED SO THE ACFT HAS RETUNED TO SERVICE.

Part: RETAINER — WEAK (PAX DOOR HANDLE) · airframe 55,394 hrs · 43,363 cycles

DURING CHECK, MAINTENANCE FOUND THE EXTERIOR HANDLE RETAINING CLIPS TENSION WEAK FOR THE TAILCONE. MAINTENANCE REPLACED THE HANDLE RETAINING CLIPS.

Part: RELEASE CABLE — DAMAGED (TAILCONE) · airframe 55,394 hrs · 43,363 cycles

DURING CHECK, MAINTENANCE FOUND THE KEVLAR ROPE ON THE TAILCONE RELEASE SYSTEM TO BE DAMAGED. MAINTENANCE REPLACED THE KEVLAR ROPE ON THE TAILCONE RELEASE SYSTEM. LP 1952047.

Part: DOOR FRAME — CORRODED (BS 650-680) · corrosion level 2 · airframe 52,123 hrs · 41,034 cycles

DURING C-CHECK, NOTED CORROSION ON LOWER MID CARGO DOOR FRAME BETWEEN BS 650-680 AROUND RIVNUTS. REPAIRED IAW SRM 53-05, FIG 125 & INSTALLED REPAIR PARTS IAW SRM 51-10-3, 53-05, FIG123.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 52,123 hrs · 41,034 cycles

DURING C-CHECK, NOTED LT ELEVATOR CONTROL TAB WAS DAMAGED AT THE TRAILING EDGE. ACCOMPLISHED BONDED REPAIR IAW SRM 51-10-2P 174 & 51-10-03. BALANCED AND REQUIRED INSPECTION PERFORMED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,754 hrs · 40,770 cycles

DURING LINE CHECK, CEILING MOUNTED EMERGENCY LIGHTS NEAR THE OVERWING EXITS WERE INOPERATIVE. REPLACED BATTERIES AND OPS CHECKED GOOD.

Part: LANYARD — BROKEN (L1 DOOR SLIDE) · airframe 51,719 hrs · 40,748 cycles

DURING LINE CHECK, L1 DOOR SLIDE COVER LANYARD WAS FOUND TO BE BROKEN. LANYARD REPLACED IAW AMM 25-62-00.

Part: SKIN — DAMAGED (BS 1235) · airframe 49,685 hrs · 39,318 cycles

SKIN DAMAGED JUST AFT OF C3 DOOR FROM FS 1235 BETWEEN L27R AND L28L. REPAIRED IAW ERA 511144-14 ORIG.

Part: DOUBLER — DAMAGED (CARGO DOOR) · airframe 49,685 hrs · 39,318 cycles

C3 CARGO DOOR SURROUND DOUBLER WAS DAMAGED AT FS 1215 TO 1219 FROM A BELT LOADER. REPAIRED IAW ERA 511117-14 ORIG.

Part: SKIN — DENTED (BS 1240) · airframe 49,685 hrs · 39,318 cycles

FUSELAGE SKIN DENTED AFT OF CARGO DOOR FS 1240 BETWEEN LONGERONS 27R TO 27L. ACCOMPLISHED DAMAGE REPAIR IAW SECTION I OF ERA 511144-14 ORG AND 511117-14 ORG.

Part: CLAMP — LOOSE (CABIN AIR) · airframe 48,886 hrs · 38,729 cycles

PERFORMED AN AIR TURN BACK, DUE TO A LOSS OF PRESSURIZATION. EXPEDITED DESCENT NO MASKS DEPLOYMENT. MX FOUND A COMPRESSOR INLET CLAMP LOOSE AT THE RT ACM AND RE-SECURED IT. ALSO FOUND THE LT PRSOV INOPERATIVE AND REPLACED IT. PERFORMED HULL LEAK CHECK AND SINGLE PACK CONFIDENCE CHECK. CHECKED GOOD.

Part: AIRSTAIR — UNKNOWN · airframe 48,736 hrs · 38,618 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND CATWALK DOWN WITH VENTRAL STAIRS DOWN. CHECKED CABLE TENSION. CHECKED GOOD, LUBRICATED DOOR, AND OPS CHECKED GOOD PER MM.

Part: TIRE — FAILED (MLG) · airframe 48,345 hrs · 38,349 cycles

AIRCRAFT BLEW NR 1 TIRE ON TAKEOFF, ALTERNATE EXTEND DUE TO LOSS OF RT HYD SYSTEM. REPLACED LT MLG DOOR, LT MLG BUNGEE CT PRESS LINE, LT MLG OTBD SPRAY DEFLECTOR, RT MLG DOOR SKID/SPACER, LT INBD TRAILING EDGE FLAP WEDGE, BOTH THE NR 1 AND NR 2 WHEEL ASSEMBLIES, LT MLG FIXED DOOR SUPPORT ROD, AND THE LT ENGINE NOSE COWL.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 45,439 hrs · 36,309 cycles

DURING TAKEOFF AND CLIMB-OUT FLIGHT ATTENDANT REPORTED SMELLING STRONG ELECTRICAL BURNING ODOR AT SEAT ROWS 27 AND 29. RETURNED TO CVG. FLIGHT ATTENDANT LATER REPORTED WATER COMING FROM CEILING, FLIGHT CREW REPORTED NO SMOKE OR ODOR IN FLIGHT DECK. MAINTENANCE ACCOMPLISHED OPN 5088 SMOKE IN CABIN TROUBLESHOOTING, REMOVED AND REPLACED OVERHEAD LIGHT BALLAST AND HARNESS AT SEAT ROW 24 ABC. COMPLIED WITH OPN 5089 PNEU SYS DUCT BURN OUT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,293 hrs · 36,195 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN FROM Y=687 TO Y=691 BTW LONGERONS 29RT TO 30 IN MID CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW ERA 491046-14 REV ORIG.

Part: FITTING — SCRATCHED (LT MLG) · airframe 45,289 hrs · 36,193 cycles

SCRATCHES ON LT MLG SUPPORT FITTING BUSHING BORE AND WEAR ON AFT WALL AT THE SAME BUSHING BORE TOO. REPAIRED PER AMR0957352 REV ORG AND ERA 491033-14AD REV ORIG.

Part: BEARING — CORRODED (LT MLG) · airframe 45,289 hrs · 36,193 cycles

SCRATCHES ON LT MLG SUPPORT FITTING BEARING BORE. REPAIRED PER AMR 0957352 REV ORG AND ERA 491033-14AD REV ORG.

Part: SKIN PANEL — CORRODED (HORIZ STAB) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON (2 EA) BARREL NUT HOLES AT LT MID UPPER SKIN PANEL OF HORIZONTAL STABILIZER AT STA XH=28. SKIN PANEL WAS REPAIRED IAW ERA 491047-14 REV ORIG.

Part: PLATE — DAMAGED (HORIZ STAB) · airframe 45,289 hrs · 36,193 cycles

DURING HMV WEAR AND CORROSION WAS FOUND ON OUTBD AND INBD LUG PLATES AT (HORIZONTAL STABILIZER PIVOT POINT) VERTICAL STABILIZER STA ZRS=173 LT. LUG PLATES WAS REPAIRED IAW SRM 55-02D PARA 24, A (1).

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER RUB STRIPS FROM STA Y=1126 TO 1127 BETWEEN LONGERONS 26RT TO 27RT, FROM STA Y=1079 TO 1092 BETWEEN LONGERONS 29RT TO 30. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53 PARA 26.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON RT MLG SUPPORT FITTING BUSHING BORE AND AFT WALL AT THE SAME BUSHING BORE TOO. SUPPORT FITTING WAS REPAIRED IAW EA 09-093855-03 AD REV B.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN BELOW RUB STRIPS BETWEEN Y=1098 TO 1104 AND LONGERON 29LT TO 28LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: RUDDER — DAMAGED (TAIL) · airframe 45,289 hrs · 36,193 cycles

DURING HMV DAMAGED METALIZED COAT WAS FOUND ON LEFT SURFACE AT RUDDER. RUDDER WAS REPAIRED IAW SRM 51-70-1AD PARA 23.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN BELOW RUB STRIPS FROM STA Y=1079 TO 1127 BETWEEN LONGERONS 26RT TO 30. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN BELOW RUB STRIPS FRON STA Y=1079 TO 1136 BETWEEN LONGERONS 20LT TO 30. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53 PARA 26.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON RT MLG SUPPORT FITTING BEARING BORE. SUPPORT FITTING WAS REPAIRED IAW EA 09-093855-03AD REV B.

Part: PLATE — WORN (VERTICAL STAB) · airframe 45,289 hrs · 36,193 cycles

DURING HMV WEAR WAS FOUND ON OUTBD SURFACE AT VERTICAL STABILIZER LUG PLATE (HORIZONTAL STABILIZER PIVOT POINT) STA ZRS=173. LUG PLATE WAS REPAIRED IAW SRM 55-02D PARA 24, A (2).

Part: SKIN PANEL — CORRODED (HORIZ STAB) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON 1 EA BARREL NUT HOLE AT RT MID UPPER SKIN PANEL OF HORIZONTAL STABILIZER AT STA XH=28. SKIN PANEL WAS REPAIRED IAW ERA 491047-14 REV ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN FROM STA Y=687 TO 691,Y=726 TO 730 AND Y=783 TO 787 BETWEEN LONGERONS 29RT TO 30 IN MID CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53 EXCEPT AT STA Y=687 TO 691 WILL BE ATTENDED WITH NRC T0203472.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON CUTOUT SETTLEMENT SURFACE OF RADIO ALTIMETER ANTENNAS (4EA). FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53 PARA 26.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON LOWER FUSELAGE SKIN BETWEEN Y=790 TO 780 BETWEEN LONGERON 29RT TO 29LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: HEATER BLANKET — CORRODED (RT WING) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON RT WING HEATER BLANKET CUTOUT EDGE OF ACCESS NBR 1409C. HEATER BLANKET WAS REPAIRED IAW ERA 490037-14AD REV ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV RUSTED FASTENERS AND CORROSION WAS FOUND ON DOUBLERS OF PREVIOUS REPAIR AT FUSELAGE SKIN BETWEEN LONG 18R-19R AND STA Y=169-200. DOUBLERS WERE REPLACED IAW ERA 333312-14 REV B.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN OF BELLY DRAIN AREA BETWEEN STA Y=1098 AND Y=1117. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.

Part: CUSP WEB — CORRODED (CABIN) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON RT CUSP WEB X=-54 TO -60 FROM STA Y=1146-1155;1171-1174;1211-1220 AND 1237-1250 AT PAX CABIN. NEW CUSP WEB WAS INSTALLED IAW SRM 53-20-02D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN SETTLEMENT SURFACE OF VHF NR 2 AND NR 3 ANTENNAS. FUSELAGE SKIN AT NR 2 ANTENNA WAS REPAIRED IAW SRM 53-04D FIG 38 AND FUSELAGE SKIN AT NR 3 ANTENNA WAS REPAIRED IAW SRM 53-04D FIG 53 PARA 26 SHEET 8.

Part: SKIN PANEL — CORRODED (HORIZ STAB) · airframe 45,289 hrs · 36,193 cycles

DURING HMV CORROSION WAS FOUND ON (2 EA) BARREL NUT HOLES BELOW NUTS AT LT MID UPPER SKIN PANEL OF HORIZONTAL STABILIZER AT STA XH=28. SKIN PANEL WAS REPAIRED IAW ERA 491047-14 REV ORIG.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 44,785 hrs · 35,862 cycles

DURING LINE CHECK MX, FOUND EMERGENCY LIGHT AT SEAT 23DE INOPERATIVE. MX RE-TERMINATED LIGHT CONNECTOR. OPS OF LIGHT NOW CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,223 hrs · 35,512 cycles

DURING SERVICE CHECK, MX FOUND OVERHEAD EMERGENCY LIGHT AT ROWS 23 THRU 26 INOPERATIVE. MX RE-LAMPED, REPLACED BATTERY, AND POWER SUPPLY B5-104. OPS OF LIGHTS NOW CHECKS OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 44,114 hrs · 35,430 cycles

DURING SERVICE CHECK MX FOUND EMERGENCY LIGHTS AT ROW 23 INOPERATIVE. MX REPLACED FIXTURE AND PIGTAIL. OPS OF LIGHTS NOW CHECKS OK.

Part: FRAME — UNKNOWN (FUSELAGE) · airframe 44,026 hrs · 35,365 cycles

FUSLEAGE MAIN FRAME LT LOWER NOSE LONGERON 22-26 AND ATTACH FRAME REPAIRED IAW EA 09-069225-12, ME01.

Part: CASE — FAILED (NR 1 STARTER) · airframe 41,591 hrs · 33,691 cycles

ON ENGINE START GOOD PRESSURE AND START VALVE BUT NO ENGINE ROTATION. FOUND LT STARTER CASE FAILED. REMOVED AND REPLACED LEFT ENGINE STARTER ASSY, CHECKS GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,479 hrs · 32,176 cycles

THE STA 1463 CANTED BULKHEAD STRUCTURE AND THE OVERLYING AFTERBODY SKIN PANEL BETWEEN THE VERTICAL STABILIZER ATTACH ANGLES WERE FOUND DAMAGED BETWEEN L-2L AND L-2R. CUT OUT DAMAGE AND INSTALLED REPAIRS TO THE BULKHEAD STRUCTURE. REMOVED AND REPLACED THE SKIN PANEL.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 39,479 hrs · 32,176 cycles

VERTICAL STABILIZER LT IN SPAR SKIN, SKIN STRAP, FWD SPAR CHORD, AND FWD SPAR WEB FOUND CRACKED. CUT OUT DAMAGE AND INSTALLED REPAIRS.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 37,871 hrs · 30,140 cycles

UPON CONFIGURING A/C FOR LANDING, LEFT HYD QUANTITY WENT TO 3 QUARTS AND REMAINED THERE. RAN QRH AND LANDED NORMALLY. DID NOT START APU AS PER QRH CHECKLIST. FOUND HYD LINE B NUT LOOSE ON LT ENG HYD CASE DRAIN FILTER OUTBOARD SIDE. RETORQUED SAME PER AMM. PERFORMED LEAK CK. ALL NML.

Part: CONNECTOR — LOOSE (CABIN) · airframe 37,434 hrs · 29,647 cycles

SECURED LOOSE EMERGENCY LIGHT HARNESS PLUG AT SEAT 31DE AND 23DE, OPS CHK GOOD.

Part: OIL CAP — LEAKING (APU) · airframe 35,617 hrs · 27,390 cycles

ATB CREW REPORTED SMOKE IN CABIN T/S SYS-REPLACED APU OIL CAP-FOUND HOLD DOWN SPRING WEAK. INSPECTED OIL SYS-TIGHTENED LOOSE B-NUT. PERFORMED OPN 508 DUCT BURNOUT. ALL OPS NML AND OPN 5088 CABIN SMOKE/ODOR T/S-ALL OPS NML.

Part: BOOT — FAILED (TAIL) · airframe 34,082 hrs · 25,941 cycles

TAIL COMPT HIGH TEMP MSG ON CLIMB-OUT. REPLACED FAILED BOOT ON MIX MANIFOLD.

Part: FAN — FAILED (E/E BAY) · airframe 29,876 hrs · 23,011 cycles

ON CLIMBOUT OF BHM TWO STANDBY RADIO RACK FAN CIRCUIT BREAKERS POPPED AT APPROX 6000 FT. THIS WAS FOLLOWED BY ELECT SMOKE SMELL IN COCKPIT AND CABIN. NO VISIBLE SMOKE PRESENT. SHORTLY AFTER THE 3RD STBY FAN CIRCUIT BREAKER POPPED. THE CREW THEN SELECTED VENTURI POSITION OF RADIO RACK COOLING AND RETURNED TO BHM. REPLACED STANDBY RADIO RACK FAN AND R2-296 RELAY.

Part: SELECTOR KNOB — JAMMED (COCKPIT) · airframe 28,486 hrs · 22,062 cycles

AFTER TAKEOFF AUTO PRESS INOP LIGHT INOP ILLUM, WENT TO MANUAL PRESS AND COULD NOT CLOSE OUTFLOW VALVE. OUTFLOW VALVE WOULD OPEN, BUT NOT CLOSE. AIR TURNBACK AIRCRAFT RETURNED TO LGA. FOUND AUTOPILOT SELECTOR KNOB JAMMED IN OUTFLOW VALVE CONTROL WHEEL IN PEDESTAL. REMOVED KNOB OUTFLOW VALVE, OPS NML IN MANUAL. RESET NR 1 AND NR 2 AUTO PRESS CONTROLLERS. AUTO NOW OPS NML. INSPECTED OUTFLOW VALVE FOUND NML.

Part: LINE — LEAKING (RT TAIL COMPT) · airframe 28,371 hrs · 21,975 cycles

RT HYD PRESSURE AND QTY WENT TO ZERO FOLLOWING LANDING GEAR EXTENSION. REPLACED LEAKING FLEX LINE FWD OUTBOARD ON RT ENGINE HYD FILTER MODULE.

Part: COALESCER BAG — CONTAMINATED (AIR DISTRIBUTION) · airframe 23,107 hrs · 18,065 cycles

F/A REPORTED SMOKE AND FUMES AFT CABIN ON CLIMBOUT. RETURNED ENOUGH TO NOTICE IN COCKPIT. FOUND NO HYD LEAKS, FOUND APU INLET CLEAN. RAN ENGINES TO TAKEOFF, NO SMOKE NOTED. REPLACED WATER SEP BAGS, PERFORMED DUCT BURNOUT. (PERFORMED OPN 5088 SMOKE/SMELL TROUBLESHOOTING).

Part: DOOR — SEPARATED (LAV SERVICE) · airframe 21,705 hrs · 17,008 cycles

AFTER TAKEOFF FROM ATL AT 10,000 FT ACCELERATING THROUGH APPROXIMATELY 280 KNOTS, FLIGHT ATTENDANT ON AFT JUMP SEAT REPORTED A SINGLE BANG FROM LEFT SIDE. AFTER LANDING, AFT SERVICE DOOR WAS MISSING. SUSPECT APPROX 20 NM NW OF KATL. RELACED AFT LAV SERVICE PANEL DOOR.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 21,548 hrs · 16,886 cycles

EMERGENCY TRACK LIGHTS INOP ON ROW 36. RECONNECTED CANNON PLUG AT SEAT 36CDE FOR EMERGENCY LIGHTS, OPS CHECKS GOOD.

Part: CONTROL VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 21,473 hrs · 16,821 cycles

ABORTED T/O DUE TO RT ENG NOT ACCELERATING TO T/O POWER. EXITED RUNWAY, TRIED TO SPOOL UP RT ENG SEVERAL TIMES AND THE RT ENG WOULD NOT ACCELERATE WITHIN TIME LIMITS. REPLACED START BLEED CONTROL VALVE. RAN ENGINE ACCEL CHECK PER PFHB. ACCEL CHECK WAS NORMAL.

Part: OVEN — CONTAMINATED (GALLEY)

CREW REPORTED, BURNING SMELL FROM FWD PORTION OF CABIN, NO SMOKE. UNABLE TO DETERMINE LOCATION/ORIGIN OF FUMES. INSPECTED CABIN OVHD AND GALLEY AREAS, STATIC PORT HEATERS, APU INLET AND OIL LEVEL. RAN PACKS WITH BOTH ENGINES. ONLY ODOR CAME FROM THE FWD GALLEY OVEN AREA. SUSPECT MEAL CARRIER MAY HAVE HAD PLASTIC DEBRIS MELTED TO EXTERIOR OF UNIT. UNPLUGGED CANNON PLUG AND PULLED/COLLARED C/B FOR OVEN. FWD TO MCO/PLAC PER MEL.

Part: SKIN — GOUGED (R-1 DOORWAY)

SKIN UNDERNEATH R-1 DOOR GOUGED ALONG L-18R. DAMAGE FOUND AT HMV1-ATL. REPAIRED BY BLENDING GOUGES AND INSTALLING REPAIR DOUBLERS.

Part: SKIN — CREASED (BS 237)

SKIN FWD OF STA 237 HAS 5 INCH CREASE BETWEEN L-18L AND L-17L. REPAIR CONSISTS OF TRIMMING OUT DAMAGE AND INSTALLING REPAIR DOUBLER.

Part: BATTERY — OVERHEAT (BATTERY COMPT)

DURING WALKAROUND NOTICED ACRID BURNING SMELL NEAR EXT POWER HOOK UP RECEPTACLE. REPLACED AIRCRAFT BATTERIES AND CHARGER.

Part: SOCKET — CORRODED (EXTERIOR)

EXTERIOR EMERGENCY RT OFF WING LIGHT INOP. CLEANED SOCKET CHECKS FINE.

Part: LIGHTS — INOPERATIVE (CABIN)

LT AND RT EMERGENCY WING EXTERIOR LIGHTS INOP.

Part: BULB — MISSING (CABIN)

EMERGENCY TRACK WHITE LIGHT AT 21 ED MISSING. REPLACED MISSING BULB AND LENS CHECKS FINE.

Part: CLAMP — LOOSE (HEAT EXCHANGER)

TAIL COMPARTMENT TEMP HIGH LIGHT IN FLIGHT. DECLARED AN EMERGENCY. FOUND DUCT LEAKING AT CLAMP ON LT HEAT EXCHANGER. SECURED CLAMP.

Part: LIGHT — MISSING (CABIN)

ONE WHITE TRACK LIGHT MISSING AT SEAT 1 CD. INSTALLED BULB AND LENS IN TRACK LIGHT AT 1 CD.

Part: LIGHT — MISSING (CABIN)

EMERGENCY TRACK LIGHT MISSING AT SEAT 1 CD. INSTALLED BULB AND LENS, OPS CHK NORMAL.

Part: TR UNIT — MALFUNCTIONED (NR 2 VHF COMM)

LOST BOTH RADIOS INFLIGHT, ALL FREQUENCIES. JAMMED WHATEVER FREQ WAS SELECTED WITH CONSTANT TRANSMISSION. ATTEMPTED ALL COMBINATIONS OF AMPS, RADIOS AND MICS TO NO AVAIL. FINAILLY SOMETHING CHANGED AND WE WERE ABLE TO ISOLATE PROBLEM TO F/O'S SIDE. ANY RADIO COPILOT SELECTED WOULD WIPE OUT THE FREQUENCY. REPLACED F/O'S AUDIO SELECT PANEL AND NR 2 VHF COMM TRANSCEIVER. CALLED DFW MTC FREQ 131.37 WITH BOTH RADIOS SELECTED TO SAME FREQ. BOTH RADIOS OP, NORMAL.