N916F

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,309 hrs · 72,271 cycles

EMERGENCY LIGHTS IN COCKPIT EXTREMELY DIM WHEN TURNED ON. REPLACED COCKPIT EMERGENCY LIGHT BATTERY PER DC9 MM 33-53-0, OPS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,960 hrs · 70,985 cycles

FUSELAGE SKIN AT LWR AFT CORNER OF MAIN DOOR JAMB CRACKED. REPAIRED PER DC9 SRM 53-05 FIG 103 PAGE 407-418 & 420. REPAIR IS CAT-B N5343 ASSIGNED INSP WITHIN 28,000 CYCLES PER SRM 51-10-5C (EDDY CURRENT).

Part: CROSSBEAM — CRACKED (PAX DOOR) · airframe 55,960 hrs · 70,945 cycles

L1 DOOR CROSSBEAM 2ND FROM TOP .5 INCH CRACK AT FWD END IN RADIUS. REPAIRED L1 DOOR CROSSBEAM, BLENDED EDGE AO PART REF DC9 SRM 53-01 FIG 1, STOPPED DRILLED CRACK PER DC9 SRM 52-05 FIG 3, HF EDDY CURRENT PER DOUGLAS SOP 51-06-07, NO CRACKS NOTED.

Part: PAN — CRACKED (CARGO DOOR) · airframe 54,095 hrs · 69,261 cycles

CRACKED INNER DOOR PAN ON AFT CARGO PIT DOOR (P/N: 5910157-5).

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,095 hrs · 69,261 cycles

FRAME HAS ELONGATED FASTENER HOLE, FS 303, L15 LEFT.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 54,095 hrs · 69,261 cycles

L1 DOOR UPPER FWD CORNER INNER DOUBLER CRACK.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 54,095 hrs · 69,261 cycles

LONGERON 30 CORROSION - FS 285.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 54,095 hrs · 69,261 cycles

UPPER CARGO DOOR OUTER SKIN DAMAGED.

Part: DOUBLER — CRACKED (FUSELAGE)

FOUND LEFT FORWARD ENTRANCE DOOR FORWARD UPPER CORNER INNER DOUBLER HAS TWO CRACKS FROM EDGE GOING FORWARD. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLERS AND FILLERS PER ECRA 916-53-030-2. (M)

Part: FRAME — CRACKED (FUSELAGE)

MZJ - FOUND STATION 897 LEFT L17 FRAME CRACKED. REPAIRED PER SRM 51-30-05, 53-03, FIGURE 32, SHT 5, AND 51-10-2, 51-10-3. (M)

Part: LONGERON — CORRODED (FUSELAGE)

MZJ - FOUND CORROSION ON LONGERON 30 NEAR STATION 290. FABRICATED AND INSTALLED REPAIR STRAP ON LONGERON 30 AT STATION 290 PER ECRA 916-53-033-2. (M)

Part: ENGINE — FAILED (RT ENGINE)

KFAR - RIGHT ENGINE FAILED IN FLIGHT. (M)

Part: BRAKE ASSY — MALFUNCTIONED (MLG)

STL - FLT 460 - WHEN CHECKING LEFT BRAKE SYSTEM DURING TAXI INTO STL, LEFT BRAKE PRESS GOES TO ZERO WHEN PEDALS DEFLECTED, AND REQUIRES PUMPING UP WITH PEDALS TO REACH 3000 PSI. REPLACED LEAKING SCHRADER VALVE AND SERVICED LT BRAKE ACCUM. (M)

Part: SEAT — MISINSTALLED (COCKPIT)

MMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91, REV C. EO APPROVED BY 8110-3 DATED 7-15-99. (X)

Part: CONNECTOR — DIRTY (LANDING GEAR)

ABQ - ON APPROACH TO KDEN, NO SAFE GEAR DOWN INDICATION, LOW APPROACH FLOWN AND TOWER REPORTED GEAR HANGING. RETURNED TO ABQ, EMERGENCY GEAR EXTENSION CHECKLIST RUN, ACCOMPLISHED LOW APPROACH AT ABQ, AND LANDED WITH 6000 LBS FUEL. CLEANED AND RESEATED DIMMER BOTTOM CANNON PLUG PER MM 32-61-00 AND OPS CHECKED NORMAL. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

STA - ABQ - LOG PAGE: F32459 - EMERGENCY EXIT LIGHTS INTERMITTENTLY ILLUMINATED IN-FLIGHT. COULD NOT DUPLICATE, CHECKED EMERGENCY BATTERY AND LIGHTS. (X)

Part: SKIN — CORRODED (BS 642)

DURING C-CHECK INSPECTION, DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE SKIN AT BS 642, LONGERON 30, BL 0.0. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATED AS REQUIRED. ACCOMPLISHED IAW EIAA, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR 916-53-016-2. (M)

Part: SKIN — CORRODED (BS 642)

DURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 INCH IN WIDTH. AFFECTED AREA WS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATED AS REQUIRED. ACCOMP IAW EIAA, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR 916-53-016-2. (M)

Part: SKIN — CORRODED (BS 642)

DURNG C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 IN WIDTH. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATED AS REQUIRED. ACCOMP IAW EIAA ENGINEERING CHANGE/REPAIR AUTHORIZATION NR 916-53-016-2. (M)

Part: SKIN — CORRODED (BS 642)

MZJ - EXFOLIATION CORROSION WAS FOUND ON THE LOWER FUSELAGE EXTERNAL SKIIN AT BS 642, LONGERON 30, AND BL 0.000. CORRODED AREA MEASURES 5.25 INCH LONG AND 4.90 INCH WIDTH. TWO EXTERNAL FINGER REPAIR DOUBLERS FABRICATED AND INSTALLED ON TRIMMED OUT AREA. AN EXTERNAL REPAIR DOUBLER FABRICATED AND INSTALLED. APPROVAL SOURCES, DOUGLAS TELEX NR MISC6900/AJC AND 8110-3 DATED 30 SEPT 1996 REF ECRA NR 916-53-016-2. (M)