N932DN

Part: WEB — DAMAGED (BS 200) · airframe 39,927 hrs · 27,140 cycles

HOLE IN FLOOR MEMBRANE JUST FORWARD OF BS 200, LBL 7. FOUND TO BE OUT OF LIMITS. REPAIRED WEB MEMBRANE IAW ERA 551879-14, REV O. (LP# 2825970)

Part: SEAT TRACK — CORRODED (BS 150-200) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN SEAT TRACK, BS 150 TO 200 RBL 7 IS CORRODED. ROUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-30-01 AND DWG 9936534, REV BW.

Part: SEAT TRACK — CORRODED (BS 150-200) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN SEAT TRACK, BS 150 TO 200 LBL 7 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-30-01 AND DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (BS 256) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FORWARD WET AREA, BS 256, RBL 22 FLOOR SUPPORT CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 5930544. REV DD.

Part: FLOOR SUPPORT — CORRODED (BS 160) · airframe 39,895 hrs · 27,123 cycles

GALLEY FLOOR SUPPORT IN FORWARD WET AREA, BS 160 RBL 19 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (BS 160) · airframe 39,895 hrs · 27,123 cycles

GALLEY FLOOR SUPPORT IN FORWARD WET AREA, BS 160, RBL 19 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05 AND DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 200) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FLOOR SUPPORT CORRODED AT BS 200 LBL 8. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BETWEEN BS 160 - 200, RBL 44. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 9936534, REV BW.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FLOORBEAM BS 200 RBL 9 TO RBL 44 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-02 AND DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 212) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FLOOR SUPPORT BS 212, RBL 12 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02 AND DWG 9936535, REV CS.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FLOORBEAM CORRODED AT BS 200, RBL 7 TO LBL 7. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-02 AND DWG 9936534, REV BW.

Part: FLOOR SUPPORT — CORRODED (BS 210) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FORWARD WET AREA LBL 20 FLOOR SUPPORT INBOARD LOBES CORRODED AT BS 210. OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-01 AND DWG 2929169, REV B.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FLOOR SUPPORT, STA 160-200, LBL 43 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-05 AND DWG 9936534.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FLOOR SUPPORT, STA 160, RBL 50 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-05 AND DWG 936534, REV BW.

Part: FITTING — CORRODED (FUSELAGE) · airframe 39,895 hrs · 27,123 cycles

MAIN CABIN FORWARD WET AREA GIRT BAR SUBFLOOR FITTING, 2 EACH, CORRODED AT R1 DOOR CUTOUT. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED 2 EACH FITTINGS IAW SRM 51-30-01 AND DWG 9936534, REV BW.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 39,895 hrs · 27,123 cycles

LEFT HAND VERTICAL STABILIZER ATTACH ANGLE CRACKED. REMOVED AND REPLACED SAME IAW SRM 51-30-05 AND DWG 5912188, REV BD.

Part: STIFFENER — CRACKED (NR 2 COWLING) · airframe 39,927 hrs · 27,140 cycles

NR 2 ENGINE NOSE COWLING FORWARD BULKHEAD HAS 1 VERTICAL STIFFENER CRACKED. REMOVED NR 2 ENGINE NOSE COWL IAW MM.

Part: STIFFENER — CRACKED (NR 1 COWLING) · airframe 39,927 hrs · 27,140 cycles

NR 1 ENGINE NOSE COWL FORWARD BULKHEAD HAS 4 VERTICAL STIFFENERS CRACKED. REMOVED AND REPLACED NOSE COWLING IAW MM.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 39,890 hrs · 27,118 cycles

FOUND CRACK ON FORWARD SIDE OF RIGHT MAIN LANDING GEAR DOOR CUT OUT. REMOVED CRACKED FRAME. INSTALLED NEW FRAME IAW DWG 5930584. (LP# 9389232)

Part: SKIN — CRACKED (MLG DOORCUTOUT) · airframe 39,890 hrs · 27,118 cycles

CRACK ON LEFT FORWARD SIDE OF MAIN LANDING GEAR DOOR CUT OUT. REPLACED FRAME IAW DWG 5930584.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 35,367 hrs · 24,380 cycles

PARACHUTE PIN IS DISENGAGED ON L1 DOOR SLIDE. R & R FWD ENTRY DOOR SLIDE IAW AMM AND JIC 2561-01358-02A.

Part: SLIDE — DAMAGED (TAILCONE) · airframe 34,617 hrs · 23,937 cycles

TAILCONE SLIDE PACK UNRAVELING. R & R SLIDE IAW AMDS 2561-4643.

Part: FRAME — CRACKED (BS 1520) · airframe 34,617 hrs · 23,937 cycles

FRAME WEB, BS 1520, CRACKED. REPAIRED IAW ERA 531910-14, SECTION I.

Part: BULKHEAD WEB — CRACKED (BS 1531) · airframe 34,617 hrs · 23,937 cycles

TAIL INTERIOR, LT VENT BOX, CANTED BS 1531 BULKHEAD WEB CRACKED. REPAIRED IAW PRI/ ERA 531910-14, REV O.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 34,617 hrs · 23,937 cycles

C3 LOWER SILL CORRODED. REPAIRED IAW PRI/ERA 531852-14, REV 3.

Part: LONGERON — CRACKED (BS 1458) · airframe 34,617 hrs · 23,937 cycles

FOUND CRACKED LONGERON 2R, AFT OF BS 1458. COMPLIED WITH PRI, FINAL ERA 531964-14, REV O.

Part: SKIN — CRACKED (BS 1531) · airframe 34,617 hrs · 23,937 cycles

FUSELAGE EXTERIOR SKIN CRACKED AT BS 1531, 15" STAIRWAY CUTOUT, RT SIDE. REMOVED DAMAGE HFEC FOR CONTAINMENT. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-001, FIG 6.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 34,617 hrs · 23,937 cycles

CORROSION FOUND IN FASTENER HOLE ON THE AFT CARGO DOOR LOWER JAMB BEAM. ERA 531852-14 SECTION I WAS ACCOMPLISHED.

Part: SKIN — DAMAGED (BS 1475) · airframe 34,617 hrs · 23,937 cycles

SKIN BS 1475. LONGERON 2L FOUND DAMAGED. REPAIRED IAW ERA 491741-14, REV A

Part: SKIN — CRACKED (BS 1475) · airframe 34,617 hrs · 23,937 cycles

CRACK FOUND ON SKIN COMMON TO LONGERON 2R JUST AFT OF BS 1475. ERA 531964-14, SECTION I WAS ACCOMPLISHED.

Part: SKATE ANGLE — CRACKED (BS 1531) · airframe 34,617 hrs · 23,937 cycles

FUSELAGE EXTERIOR VERTICAL STABILIZER SKATE ANGLE CRACKED AND RIVET POPPED, CANTED BS 1531, RT SIDE. COMPLIED WITH PRI 531878-14, REV O.

Part: SKIN — CRACKED (BS 1486) · airframe 34,617 hrs · 23,937 cycles

AFT FUSELAGE SKIN, BELOW RAM AIR INLET, CRACKED BS 1486, STRINGER 2L. REPAIRED IAW PRI 491741-14, REV A.

Part: WEB — DAMAGED · airframe 33,172 hrs · 23,031 cycles

BS 101.55 CAPTAIN`S SIDE ELEVATOR CABLE FEED THROUGH AND WEB DAMAGED. REPAIRED IAW ERA 526158-14, REV O.

Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 33,104 hrs · 22,989 cycles

PERFORMED AN IN FLIGHT SHUTDOWN AND AN AIR TURN BACK DUE TO LT ENGINE OIL QUANTITY LOSS WITH OIL QTY INDICATION AT ZERO. MAINTENANCE FOUND OIL IN COWLING AND ON ENGINE. ENGINE CHANGE REQUIRED DUE TO ENGINE OPERATION WITH NO OIL PRESSURE FOR 3 MINUTES.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 32,932 hrs · 22,869 cycles

DURING SERVICE CHECK, FOUND L1 DOOR SLIDE PINS PULLED FROM SLIDE PACK COVER. R & R L1 DOOR SLIDE.

Part: RELEASE CABLE — PULLED (COCKPIT DOOR) · airframe 32,118 hrs · 22,370 cycles

DURING SERVICE CHECK, COCKPIT DOOR RELEASE CABLES PULLED OUT OF DOOR HINGES. MAINTENANCE R & R UPPER AND LOWER COCKPIT DOOR HINGE CABLES IAW AMM. OPERATION CHECKS GOOD.

Part: BOTTLE — OUT OF TOLERANCE (TAILCONE SLIDE) · airframe 31,677 hrs · 22,088 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE EVACUATION SLIDE DISCHARGE BOTTLE PRESSURE OUT OF RANGE. MAINTENANCE REMOVED AND REPLACED TAILCONE SLIDE.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 31,473 hrs · 21,951 cycles

FIRST CLASS GALLEY OVEN STARTED SMOKING WHEN IT WAS TURNED ON. MX INSPECTED CONTENTS OF OVEN, NO SPILT FOOD OR SAUCE. FD TO MCO/PLAC IAW MEL 25-34-02. CIRCUIT BREAKER PULLED AND COLLARED. PERFORMED VISUAL INSPECTION OF OVEN. FOUND COOKED MEALS IN THE OVEN, EVEN WITH CB PULLED AND COLLARED. REMOVED COLLAR FROM CB. OPERATION OF OVEN CHECKS GOOD. NO SMOKE WHEN OPERATED. OK FOR SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 31,183 hrs · 21,789 cycles

AFT F/A WITNESSED SMOKE AND ELECTRICAL ODOR FROM OVERHEAD LAST ROW OF SEATS. MX FOUND CEILING LIGHT BALLAST FORWARD END AT 37CDE BURNED/SHORTED TO MOUNT SCREW. R & R BALLAST IAW MM. OPS CHECKED NORMAL.

Part: OVEN — INOPERATIVE (FWD GALLEY) · airframe 30,730 hrs · 21,537 cycles

FORWARD GALLEY OVEN, SMALL AMOUNT OF SMOKE OMITTED VERY HOT. OVEN OFF. INSPECTED FORWARD GALLEY OVEN AND CIRCUIT BREAKER PANEL. NO TROUBLE FOUND. PULLED FOWARD GALLEY OVEN CIRCUIT BREAKER AND ISOLATED OVEN. OVEN IS NOW COOL WITH NO POWER TO IT FWD TO NEF 25-34-02. R & R OVEN ASSY. OPS CHECKS OK.

Part: SHEAR TIE — BENT (BS 237) · airframe 30,297 hrs · 21,298 cycles

SHEAR TIE AT STA 237 BENT BETWEEN L17 AND L18. REMOVED SHEAR TIE. STRAIGHTENED HFEC INSPECTED FORMER. NO CRACKS. REPAIRED IAW ERA 514591-14. INSTALLED IAW DWG 9911524.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 30,297 hrs · 21,298 cycles

FUSELAGE SKIN AFT OF L1 DOOR PUNCTURED BETWEEN L17L AND L18L. REMOVED DAMAGED SKIN IAW SRM 53-30-01. FABRICATED, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-30-01, FIG 8B.

Part: STRUCTURE — CRACKED (BS 1475) · airframe 30,169 hrs · 21,227 cycles

CEILING CLIP CRACKED AT 12 O'CLOCK POSITION AT BS 1475. REMOVED AND REPLACED CLIP IAW DWG PL 9964460.

Part: RELEASE MECH — OUT OF TOLERANCE (TAILCONE) · airframe 29,717 hrs · 20,957 cycles

DURING TAILCONE FUNCTIONAL CHECK STEP 4 OF AMDS CARD 5352-7116, MX FOUND TAILCONE RELEASE OUT OF LIMITS. RELEASED TO HIGH. ADJUSTED CLIPS ON TEE PIN AND PULL HANDLE INTERIOR. LUBED TAILCONE. PULLED WITHIN LIMITS IAW AMDS CARD. OPS CHECKED GOOD.

Part: WEB — CRACKED (BS 964) · airframe 29,717 hrs · 20,957 cycles

CANTED FRAME BS 964 WEB AFT SIDE CRACKED. 6 INCHES ABOVE LT VENT BOX AT TOP FASTENER. VERIFIED WITH HFEC. REMOVED DAMAGE. CONTAINED. FABRICATED REPAIR DOUBLER, TRIPLER AND FILLER. DRILLED AND INSTALLED IAW SRM 53-10-03, FIG 13.

Part: D-RING — WORN (DOOR SLIDE) · airframe 29,717 hrs · 20,957 cycles

SLIDE D-RINGS ATTACHED AT AFT VENTRAL WALKWAY WORN-FRAYED. R & R SLIDE D-RINGS ATTACH STRAPS AT AFT VENTRAL STAIRWAY IAW AMM. OPS CHECKS GOOD.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 29,717 hrs · 20,957 cycles

PILOTS SLIDING WINDOW FRAME CRACKED AT AFT UPPER CORNER. GAINED ACCESS, REMOVED CRACKED DOUBLER IAW 06-10.001. FOUND OK. BACK DRILLED DOUBLER, TRIMMED TO FIT, PRIMED AND INSTALLED DOUBLER IAW DWG5754688.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 26,763 hrs · 19,359 cycles

DURING HMV FOUND MID LOWER CARGO COMPARTMENT DOOR JAMB HAS SURFACE CORROSION. ACCOMPLISHED REPAIR IAW MD SRM 53-60-02 FIG 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,763 hrs · 19,359 cycles

DURING HMV FOUND MAIN CABIN SEAT TRACK AT STA 237 TO 243 LBL 44 HAS CORROSION. REPAIRED PER SRM 53-40-01 FIG 6.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 26,763 hrs · 19,359 cycles

DURING HMV IN MIA FOUND MID LOWER CARGO COMPARTMENT DOOR JAMB HAS SURFACE CORROSION AT SEVERAL PLACES. REMOVED CORROSION AND FOUND OUT OF LIMITS, ACCOMPLISHED REPAIR AT MID CARGO DOOR JAMB AND REPLACED FLOOR SUPPORT BETWEEN STA 674 AND 769 L29R IAW MD90 SRM 53-60-02, 51-30-02 AND 51-30-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 26,763 hrs · 19,359 cycles

THE CUSP WEB WAS FOUND TO BE CRACKED AT STA 218 LBL 45.5. THE WEB WAS REPAIRED IN ACCORDANCE WITH SRM 53-20-02 FIG 7 AND WAS TAGGED PER P/S NO 900-5-1 NR 04.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 26,763 hrs · 19,359 cycles

LEFT CABIN CUSP WEB CRACKED STA 1344 TO 1364. INSTALLED DOUBLER PER SG DWG SG09530019.

Part: PYLON — UNKNOWN (RIGHT) · airframe 26,763 hrs · 19,359 cycles

COMPLY WITH EA 02-476701-12 REV D OP 0301.

Part: CUSP WEB — CRACKED (CABIN) · airframe 26,763 hrs · 19,359 cycles

HMV2 LT CABIN CUSP WEB CRACKED STA 1344 - 1364 LT SIDE. REPAIRED PER BOEING SG DRAWING SG09530019.

Part: WEB — CRACKED (FUSELAGE) · airframe 26,763 hrs · 19,359 cycles

HMV2 FWD ENTRY DOOR STA 206 STGR 15L WEB CRACKED. REPAIRED PER MD90 SRM 51-30-05 AND BOEING DRWG 5956879.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,740 hrs · 19,344 cycles

STA 541 L18L LIGHTNING STRIKE REPAIR IAW SRM 53-30-01, PARA 10 AND BOEING MESSAGE BNI-BNI-10-0081-07B AND DWG SG 09530008.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,740 hrs · 19,344 cycles

NEW SKIN SECTION SPLICE IN BETWEEN LOCATIONS STA Y=229 AND SPLICE IN FRAME BAY STA Y=275 AND Y=294 IAW SRM 53-30-01 FIG 5 REF A10690.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,205 hrs · 17,617 cycles

AFT FUSELAGE RT SIDE STA CANT 1554-1567 REPAIRED IAW BOEING REPAIR SKETCH 200906050006-0003 (DE 1029120).