N928AX

Part: ROLLER — OUT OF ADJUST (MLG) · airframe 47,424 hrs · 39,647 cycles

ON TAKEOFF, RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR HANDLE PLACED IN UP POSITION. GREEN SAFE LIGHT WAS NOT ILLUMINATED. AC FELT LIKE GEAR WAS UP. RECYCLED GEAR DOWN (SHOWED NORMAL INDICATION) THEN BACK UP AND GEAR UNSAFE LIGHT WENT OUT. DEFERRED IAW FERRY PERMIT NR 022-05 AND GMM 07-04 FOR TRACKING AND GMM 04-04 CODE 05. CLEARING ACTION: FOUND RT MLG DOOR FAILED (GO) GAUGE CHECK. ADJUSTED RT MLG DOOR LATCH ROLLER IAW MM32-31-04-2-0101 STEP 4.A (5) (A) OPS CHECKED GOOD. PERFORMED TEST OF LANDING GEAR POSITION AND WARNING IAW 32-60-00-2-0101 STEP 2.A.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,657 hrs · 38,903 cycles

CRACKED MAIN ENTRY DOOR FRAME WEB AT STA 207. REPAIRED WEB IAW DC-9 SRM 51-70-4.

Part: ROLLER — OUT OF ADJUST (RT MLG DOOR) · airframe 45,816 hrs · 38,040 cycles

FOUND GEAR UPLATCH CHECK GEAR DOOR OPEN LIGHT AND RIGHT MAIN UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR AS PER ABNORMAL PROCEDURE. GEAR UPLATCH CHECK SATISFACTORY. UPON INSPECTION, FOUND RIGHT UPLATCH ROLLER NEEDED ADJUSTED. ADJUSTED DOOR ROLLER CLEARANCES AND PERFORMED UPLATCH ADJUSTMENT TEST IAW DC-9 AMM 32-60-0. OPS CHECKED GOOD AND INDICATION GOOD. UPLATCH TEST OKAY.

Part: FITTING — CRACKED (RT TE FLAP) · airframe 45,620 hrs · 37,830 cycles

RT FLAP INTERIOR FITTING AT INBOARD SIDE OF CENTER HINGE WAS CRACKED IN TWO PLACES BETWEEN RIVETS, BOTH ON UPPER SIDE OF FITTING. REPAIRED FITTING IAW DC-9 SRM 57-09.

Part: FITTING — CRACKED (LT TE FLAP) · airframe 45,620 hrs · 37,830 cycles

LEFT FLAP INBOARD HINGE, INTERNAL HINGE ATTACH FITTING WAS CRACKED ON THE OUTBOARD AFT CORNER. REMOVED AND REPLACED FLAP IAW DC-9 MM 27-51-01-4-0201.

Part: DOWNLOCK SWITCH — FAILED (NLG) · airframe 45,499 hrs · 37,710 cycles

NOSE LANDING GEAR SAFE LIGHT TOOK SEVERAL MINUTES TO ILLUMINATE AFTER SELECTING GEAR DOWN. RESULTING IN A MISSED APPROACH. THE GEAR SAFE LIGHT THEN ILLUMINATED. REPLACED THE NOSE LANDING GEAR DOWN LOCK SWITCH IAW MM. OPS CHECKED GOOD.

Part: CONTACTOR — DAMAGED (NLG IND LIGHT) · airframe 45,492 hrs · 37,701 cycles

ON DESCENT, NOSE GEAR UNSAFE LIGHT WAS INTERMITTENT WITH THROTTLES AT IDLE. CREW REPORTED CYCLED GEAR, CHECKED GOOD. FOUND NOSE GEAR LIGHT BULB POSITIVE CONTACT FLATTENED AND MUSHROOMED CAUSING INTERMITTENT INDICATION. REPAIRED CONTACT. OPS CHECKED GOOD IAW AMM.

Part: DOUBLER — CRACKED (BULKHEAD) · airframe 44,471 hrs · 36,654 cycles

AFT PRESSURE BULKHEAD CENTERLINE FINGER DOUBLER WAS CRACKED AND HAD A PIECE MISSING ON THE FORWARD SIDE OF BULKHEAD. REPAIRED AREA IAW REA D953-41525.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,471 hrs · 36,654 cycles

FLOORBEAM AT STA 965, LEFT BUTT LINE 45 WAS CORRODED ON AFT SIDE THROUGH LIGHTENING HOLE. REPAIRED FLOORBEAM IAW REA D953-41486MR.

Part: RETAINER — CRACKED (CABIN) · airframe 44,471 hrs · 36,654 cycles

CRACK AT LOWER AFT FASTENER OF WINDOW RETAINER, FS 658 AND LONGERON 15 RIGHT. REPAIRED AREA IAW DC-9 SSRM K07226.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,471 hrs · 36,654 cycles

FORWARD SIDE OF FLOORBEAM WEB EXFOLIATED AT FS 389, AT APPROXIMATELY LEFT BUTT LINE 48. REPAIRED FLOORBEAM AT FS 389, LEFT BUTT LINE 48 IAW REA D953-41479. MATERIAL REMOVED WAS APPROXIMATELY 1 - 2 INCHES.

Part: SPLICE — DAMAGED (FUSELAGE) · airframe 44,471 hrs · 36,654 cycles

DURING C-CHECK, THE AFT PRESSURE BULKHEAD SPLICES WERE FOUND TO HAVE ELONGATED HOLES. REPAIRED AFT PRESSURE BULKHEAD TEE CAP SPLICES IAW REA D953-41487MR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,471 hrs · 36,654 cycles

AFT LEFT MAINFRAME AT STA 737 WAS CRACKED IN THE AFT FLOORBEAM POCKET UPPER FLANGE. VERIFIED WITH EDDY CURRENT INSPECTION. REPAIRED MAINFRAME IAW DC-9 EA 53400310-001-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,471 hrs · 36,654 cycles

FORWARD RIGHT MAINFRAME AT STA 699 WAS CRACKED IN THE FORWARD FLOORBEAM POCKET UPPER FLANGE. VERIFIED WITH EDDY CURRENT INSPECTION. INSTALLED REPAIR DOUBLER IAW DC-9 EA 53400120-1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,471 hrs · 36,654 cycles

UPPER CARGO FLOOR FRAME AT STA 965 WAS HEAVILY CORRODED FROM LONGERON 26 LEFT OUTBOARD TO LONGERON 22 LEFT. REPAIRED IAW REA D953-41486MR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,471 hrs · 36,654 cycles

UPPER AND LOWER SPLICE CHANNELS IN FRAME AT STA 937 WAS HEAVILY CORRODED AND BULGING ABOVE LONGERON 28 LEFT AND LONGERON 27 LEFT. REPLACED FRAME AT STA 937, LONGERON 28 TO LONGERON 25 LEFT IAW DC-9 SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,471 hrs · 36,654 cycles

FUSELAGE SKIN DENTED AT STA 353 BETWEEN LONGERON 21 AND 22 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR.

Part: RETAINER — CRACKED (CABIN) · airframe 44,471 hrs · 36,654 cycles

CRACK AT RADIUS OF FORWARD LOWER CORNER OF WINDOW RETAINER, FS 598 AND LONGERON 15 RIGHT. REPAIRED WINDOW RETAINER ON LOWER CORNER AT FS 598 AND LONGERON 15 RIGHT IAW DC-9 SRM DWG K07226.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,471 hrs · 36,654 cycles

FUSELAGE SKIN CREASED AT STA 358 BETWEEN LONGERONS 21 RIGHT AND 22 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR. CUTOUT WAS 2.1 INCH IN DIAMETER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,471 hrs · 36,654 cycles

FLOORBEAM LOWER FORWARD ANGLE CORRODED AT FS 965 LT, LBL 22-44. REPAIRED AREA IAW REA D953-41486MR.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,471 hrs · 36,654 cycles

REPAIR ON FUSELAGE SKIN DENTED AT STA 346, LONGERON 21 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN IAW REA D953-41469MR.

Part: INTERCOSTAL — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INTERNAL INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1.

Part: SHEAR TIE — CRACKED (VERT STAB)

DURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH FITTING SHEAR-TIE AT STATION 1094 CRACKED. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (VERT STAB)

DURING C-CHECK, FOUND VERTICAL STABILIZER LEFT ATTACH FITTING CRACKED AT STATION 1094. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: PAN — CRACKED (FWD LWR CARGO)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT THIRD STOP FROM TOP AFT FLANGE. REPAIRED PAN IAW DC9 SRM 52-05.

Part: END CAP — CORRODED (AFT LWR CARGO)

DURING C-CHECK, FOUND LONGERON 30 END CAP CORRODED AT STATION 986 TO 996. REPLACED END CAP IAW DC9 SRM 51-30-5.

Part: PANEL — DELAMINATED (LT WING)

DURING C-CHECK, FOUND LEFT WING TRAILING EDGE PANEL 1507 DELAMINATED AT INTERIOR HINGE. REPLACED PANEL IAW DC9 SRM 51-30-1.

Part: ROD — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR LOCK ROD FLANGE CRACKED. REPAIRED LOCK ROD IAW DC9 MM 52-30-1.

Part: PAN — CRACKED (FWD LWR CARGO)

DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR OUTER PAN CRACKED IN 6 PLACES. REPAIRED IAW ABX REA D952-33773.

Part: INTERCOSTAL — CRACKED (BS 579-593)

DURING C-CHECK, FOUND INTERCOSTAL CRACKED BETWEEN STATION 579-593 AT LONGERON 9 RIGHT. REPAIRED IAW DC9 SRM 53-01.

Part: RIB — CRACKED (RIGHT WING)

DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE PANEL INBOARD RIB CRACKED OUTBOARD OF MAIN LANDING GEAR. REPLACED RIB IAW DC9 SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (FWD LWR CARGO)

DURING C-CHECK, FOUND FORWARD LOWER CARGO COMPARTMENT DOOR INTERNAL INTERCOSTAL AT LOWER DOOR STOP CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1.

Part: ANGLE — CRACKED (NR 2 NACELLE)

DURING C-CHECK, FOUND NR 2 ENGINE PYLON UPPER ATTACH ANGLE CRACKED AT STATION 950. REPAIRED ANGLE IAW DC9 SRM 54-04.

Part: WINDOW — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND LEFT FORWARD EMERGENCY EXIT OUTER WINDOW PANE CRACKED COMPLETELY THROUGH. REPLACED WINDOW IAW DC9 MM.

Part: BULKHEAD CLIP — CRACKED (AFT PRESS BLKHD)

AFT PRESSURE BULKHEAD RADIAL STIFFENER 16 LEFT ATTACH CLIP CRACKED ADJACENT TO LONGERON 18 LEFT. REPLACED CLIP IAW DC9 SRM 51-30-5.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY LIGHTS WOULD NOT ARM. CAME ON INITIALLY, THEN FADED. REPLACED BATTERIES, OPS CHECKED GOOD.

Part: LATCH — BROKEN (COCKPIT)

COCKPIT DOOR WOULD NOT OPEN. REPAIRED COCKPIT DOOR LATCH.

Part: LATCH — BENT (COCKPIT DOOR)

COCKPIT DOOR WAS STUCK CLOSED. WOULD NOT OPEN. FOUND LATCH TO BE BINDING. REPAIRED AND REASSEMBLED HANDLE.

Part: FITTING — CRACKED (BS 604)

DURING C-CHECK, FOUND LONGERON 29R FITTING CRACKED AFT OF STATION 604. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FRAME — CRACKED (BS 980)

DURING C-CHECK, FOUND FRAME AT STATION 980 AND LONGERON 16L AND 17L CRACKED AT HI-LOK. REPAIRED IAW DC9 SRM 53-03.

Part: FITTING — CRACKED (BS 604)

DURING C-CHECK, FOUND LONGERON 28L END FITTING CRACKED AFT OF STATION 604. REPLACED LONGERON FITTING IAW DC9 SRM 51-30-5.

Part: SKIN — CORRODED (BS 439)

DURING C-CHECK, FOUND FUSELAGE SKIN AT STATION 439 BETWEEN LONGERON 30 AND LONGERON 29L BULGED AND CORRODED BEYOND LIMITS. REPAIRED SKIN IAW DC9 SRM 53-04.

Part: LONGERON — CORRODED (BS 965)

DURING C-CHECK, FOUND LONGERON 16R CORRODED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: FITTING — CRACKED (BS 579)

DURING C-CHECK, FOUND LONGERON 29L FITTING CRACKED JUST FWD OF STATION 579. REPLACED END FITTING IAW DC9 SRM 51-30-1.

Part: FITTING — CRACKED (BS 604)

DURING C-CHECK, FOUND LONGERON 26R END FITTING CRACKED AFT OF STATION 604. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (BS 604)

DURING C-CHECK, FOUND LONGERON 29L END FITTING CRACKED AFT OF STATION 604. REPLACED END FITTING IAW DC9 SRM 51-30-5.

Part: FRAME — CRACKED (BS 637)

DURING C-CHECK, FOUND FRAME AT STATION 637 CRACKED IN THE LEFT KEEL BEAM ON THE OUTBOARD END. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: FITTING — CORRODED (BS 907)

DURING C-CHECK, FOUND INTERCOSTAL CORRODED IN AFT LOWER CARGO DOOR JAMB POCKET AT STATION 907 AND LONGERON 28R. REPLACED INTERCOSTAL TEE FITTING IAW DC9 SRM.

Part: LONGERON — CORRODED (BS 869)

DURING C-CHECK, FOUND CORROSION ON THE UNDERSIDE OF LONGERON 29R AT STATION 869. REPAIRED LONGERON IAW ABX REA D953-23023-MR.

Part: LONGERON — CRACKED (BS 408/427)

DURING C-CHECK, FOUND LONGERON 29L CRACKED BETWEEN STATION 408 AND 427. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 130-160)

DURING C-CHECK, FOUND LONGERON 25R CORRODED BETWEEN STATION 130 AND 160. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 16L CRACKED AT HI-LOK AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND SHEAR TIE CRACKED IN RADIUS AT STATION 945 BETWEEN LONGERON 15R AND 16R. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2.

Part: ANGLE — CRACKED (LT TE FLAP)

DURING C-CHECK, FOUND ATTACH ANGLE INSIDE LEFT FLAP CRACKED, ACCESS THROUGH PANEL 1548. REPLACED ATTACH ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHTS BATTERIES.

Part: FAIRING — CRACKED (NR 1 TR UNIT)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-07, FOUND NR 1 REVERSER UPPER DOOR INBOARD FAIRING CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-8.

Part: FITTING — MISDRILLED (WS 267)

DURING C-CHECK, FOUND A .1875 INCH HOLE DRILLED THROUGH THE UPPER SURFACE OF THE WING INBOARD FLAP ATTACH FITTING. REPAIRED IAW ABX REA D957-15559-MR.

Part: FAIRING — CRACKED (NR 2 TR UNIT)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND NR 2 REVERSER UPPER DOOR OUTBOARD FAIRING CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-8.

Part: FORMER — CRACKED (RT TE FLAP)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT FLAP OUTBOARD FLAP ATTACH FITTING CRACKED. REPLACED IAW DC-9 SRM 51-30-1, 51-30-2.

Part: BRACKET — CRACKED (LT TE FLAP)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT FLAP ATTACH BRACKET CRACKED AT STATION 353. REPLACED IAW DC-9 SRM 51-30-4, 51-30-1, 51-30-2.

Part: MOUNT STRAP — CRACKED (NR 1 ENGINE)

NR 1 ENGINE, REAR ENGINE MOUNT CRACKED OFF BETWEEN VIBRATION ISOLATOR AND FUSELAGE. REPLACED CRACKED MOUNT STRAP PER SRM 51-50-1 AND 51-30-5.

Part: DOUBLER — CRACKED (LT EYEBROW)

DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, FOUND CRACKS AROUND FASTENER HOLES ON THE LEFT OVERHEAD EYEBROW WINDOW CORNER, LEFT SIDE DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: DOUBLER — CRACKED (RT EYEBROW)

DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, FOUND CRACKS AROUND FASTENER HOLES ON THE RIGHT OVERHEAD EYEBROW WINDOW CORNER, LEFT SIDE DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: BUSHING — MISSING (RT MLG DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING MISSING IN RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.