N563PC
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
96 reports on file, 1995-02-16 – 2010-08-19.
Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
DURING INSP LOWER FUSELAGE UNDER WING TO FILLET FAIRING CHANNEL WITH CORROSION FROM STA Y523 TO STA Y547 BTWN LONG 28L AND LONG 29L.
Part: EXHAUST DUCT — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
DURING INSP ENGINE NR2 EXHAUST DUCT WITH SPOT CORROSION AT L/E SKIN.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
DURING INSP UPPER FUSELAGE PAX CABIN AT STA Y503 AND STA Y525, +X33 FLOOR CHANNEL WITH CORROSION.
Part: SKIN — DENTED (ZONE 100) · airframe 56,594 hrs · 69,840 cycles
DURING INSP EXTERNAL FUSELAGE SKIN WITH DENT AT BS 436.5 BTWN LONG 19L AND LONG 20L.
Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 56,594 hrs · 69,840 cycles
DURING INSP EMPENNAGE HORIZ STABILIZER BTWN XFS 221 AND XFS 235 RT ELEVATOR FRONT SPAR WITH CRACKS.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y408, LONGERON 15 RT FRAME WITH DOUBLE HOLE.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 52,704 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y446 BETWEEN LONG 9 RT AND LONG 11 RT FRAME WITH DOUBLE HOLES.
Part: FITTING — CRACKED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE PAX CABIN AT STA Y503 +X22, -Z2 FITTING CRACKED.
Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE CARGO CABIN AT STA Y680, +X33, Z0 SUPPORT CHANNEL WITH CORROSION.
Part: LONGERON — CRACKED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
CARGO CABIN AT STA Y160, LONG 4L WITH CRACK.
Part: FRAME — DAMAGED (ZONE 200) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y370, LONGERON 15 RT FRAME WITH DOUBLE HOLE.
Part: FRAME — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y294, LONGERON 15 RT FRAME AND STRAP WITH DOUBLE HOLES.
Part: FRAME — DAMAGED (ZONE 100) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y237 LONGERON 11 RT FRAME WITH DOUBLE HOLES.
Part: FRAME — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y313 BETWEEN LONG 10R AND LONG 11R FRAME WITH DOUBLE HOLES.
Part: SKIN — BULGED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
LOWER FUSELAGE SKIN WITH BULGED AT STA Y490.540 BETWEEN LONG 29L AND LONG 29R.
Part: SPOILER — DELAMINATED (LT WING) · airframe 56,594 hrs · 69,840 cycles
LEFT WING OUTBOARDD FLIGHT SPOILER P/N 5910055-513, S/N 13033 DELAMINATED.
Part: SKIN — DENTED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE EXTERIOR FUSELAGE SKIN WITH DENT AT STA Y933 BETWEEN LONG 6L AND LONG 7L.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y427 LONGERON 15 RT FRAME WITH DOUBLE HOLE.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE CARGO CABIN STA Y786 LONGERON 12 RT CRACKED.
Part: FRAME — DAMAGED (ZONE 200) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y465 LONGERON 15 RT FRAME WITH DOUBLE HOLE.
Part: FRAME — DAMAGED (ZONE 100) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y275 LONG 15 LT FRAME WITH ELONGATED HOLE.
Part: PANEL — DELAMINATED (RT WING) · airframe 56,594 hrs · 69,840 cycles
RIGHT WING T/E UPPER FIXED PANEL P/N 5912737-2 DELAMINATED.
Part: SKIN — DENTED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
EXTERNAL FUSELAGE SKIN WITH DENT AT BS 436.5 BETWEEN LONG 19L AND LONG 20L.
Part: FRAME — CRACKED (ZONE 200) · airframe 56,594 hrs · 69,840 cycles
TAIL COMPARTMENT AT STA Y925.937 CANT, LONG 16L FRAME WITH CRACK.
Part: SPAR CAP — CRACKED (LT WING) · airframe 56,594 hrs · 69,840 cycles
LEFT WING FRONT SPAR STA XCW 58.5 UPPER CAP WITH CRACK.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE CARGO CABIN STA Y786 LONG 12 LT CRACKED.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE PAX CABIN AT Y623 +X50 FLOOR CHANNEL WITH CRACK.
Part: PANEL — DELAMINATED (RT WING) · airframe 56,594 hrs · 69,840 cycles
RIGHT WING T/E UPPER FIXED PANEL P/N 5912735-2 DELAMINATED.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
LOWER FUSELAGE STA Y465 LONG 21 LT CRACKED.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
TAIL COMPARTMENT AT STA Y964.019 CANT FRAME WITH CRACK AT STAIRWAY ACTUATOR SUPPORT FITTING AREA.
Part: SKIN — CORRODED (ZONE 100) · airframe 56,594 hrs · 69,840 cycles
LOWER FUSELAGE SKIN CORRODED FROM STA Y643 TO STA Y718 BETWEEN LONG 18L AND LONG 29L.
Part: SKIN — CRACKED (ZONE 100) · airframe 52,704 hrs · 69,840 cycles
AFT UNPRESSURE FUSELAGE STA Y988 CANT AT +X28 AND Z23 SKIN WITH CRACK.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
AFT UNPRESSURE FUSELAGE STA Y964 ON LEVEL LONG 19L SKIN WITH CRACK.
Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE CARGO CABIN AT STA Y680, +X33, Z0 SUPPORT CHANNEL WITH CORROSION.
Part: FRAME — WORN (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y275 BETWEEN LONG 14R AND LONG 15R AND LONG 17R AND LONG 18R FRAME WORN.
Part: FRAME — DAMAGED (ZONE 200) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y370, LONGERON 15 RT FRAME WITH DOUBLE HOLE.
Part: FRAME — CRACKED (BS 680 L13-14R) · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE CARGO CABIN STA Y680 BETWEEN LONG 13R AND LONG 14R.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE CARGO CABIN STA Y718 BETWEEN LONG 17 LT AND LONG 18 LT FRAME WITH DOUBLE HOLE.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE PAX CABIN STA Y786 +X50, -Z4 FLOORBEAM WEB WITH CORROSION.
Part: LONGERON — CRACKED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE PAX CABIN AT STA 160 LONGERON 3L RADIUS WITH CRACK.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y389, LONGERON 15 RT WITH DOUBLE HOLE.
Part: FRAME — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN AT STA Y332 BETWEEN LONG 10 RT AND LONG 11 RT FRAME WITH DOUBLE HOLES.
Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO CABIN FROM STA Y200 TO STA Y218, -X48, Z0 FLOOR MEMBRANE WITH CORROSION.
Part: FRAME — DAMAGED (ZONE 100) · airframe 56,594 hrs · 69,840 cycles
MAIN CARGO AT STA Y206 BETWEEN LONG 16R AND LONG 17 RT FRAME RADIUS WITH HOLE.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,594 hrs · 69,840 cycles
UPPER FUSELAGE PAX CABIN STA Y786, +X50, -Z4 FLOORBEAM WEB WITH CORROSION.
Earlier reports · 1995–2007 · 51 reports
2007
Part: GUSSET — CRACKED (BULKHEAD) · airframe 55,480 hrs · 69,225 cycles
PASSENGER AFT ENTRANCE DOOR AFT PRESSURE BULKHEAD CUTOUT LOWER LEFT CORNER LEAKED AND SHOWED EVIDENCE OF A CRACK IN THE DOUBLERS. REPAIRED LOWER AFT PRESSURE BULKHEAD IAW REA D953-56099-MR. P/N'S: 5910130-85/87, CRACK LENGTHS: 2.250" AND 1.625".
2000
Part: DOUBLER — CRACKED (WINDOW FRAME)
DURING INSPECTION PER SB 56-11 A CRACK WAS FOUND IN UPPER AFT CORNER OF THE LEFT COCKPIT SLIDING WINDOW FRAME INTERNAL DOUBLER. THE AIRCRAFT WAS FERRIED FROM FWA TO DFW FOR REPAIRS. THE DOUBLER WAS REMOVED AND REPLACED PER THE DC-9 SRM AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: DOUBLER — CRACKED (WINDOW FRAME)
DURING INSPECTION PER SB 56-11 A CRACK WAS FOUND IN UPPER AFT CORNER OF THE LEFT COCKPIT SLIDING WINDOW FRAME INTERNAL DOUBLER. THE AIRCRAFT WAS FERRIED FROM FWA TO DFW FOR REPAIRS. (M)
1999
Part: INTERCOSTAL — CORRODED (BS 710 TO 718)
DURING C-CHECK INSPECTION, FOUND CORROSION ON THE INTERCOSTAL FROM STA 710 TO STA 718 BETWEEN L29L TO L30. THE INTERCOSTAL WAS REPLACED IAW DC-9 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)
Part: CONNECTOR — DIRTY (BRAKE)
FLT 563 - EWR-DFW - AFTER LANDING AT DFW ON ROLL OUT THE LEFT BRAKE WOULD NOT APPLY. THE BRAKE OPERATED NORMALLY WITH THE ANTI-SKID OFF. THE AIRCRAFT TAXIED TO PARKING WITHOUT INCIDENT. CLEANED CANNON PLUG ON BOTH DUAL SERVO VALVES IN LEFT WHEEL WELL. OPS CHECK ON GROUND SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SKIN — DENTED (LT TE FLAP)
DURING C-CHECK INSPECTION, FOUND NUMEROUS DENTS ON THE LEFT FLAP REMOVABLE PANEL TRAILING EDGE SKIN AT XFLS 65.5 TO XFLS 127.4. THE SKIN WAS REPLACED IAW KITTY HAWK EA D9-57-008, THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
1998
Part: CONTROL CABLE — LOOSE (RT MLG WW)
KHA - FLT 1211 - YIP-MMLO - AFTER TAKEOFF FROM YIP THE FLIGHT CREW FOUND THE LANDING GEAR DID NOT RETRACT WITH THE GEAR HANDLE UP. THE CREW ELECTED TO RETURN TO YIP AND MADE AN UNEVENTFUL LANDING. INVESTIGATION FOUND THE LANDING GEAR BY-PASS HANDLE CABLE OFF A PULLEY KEEPING THE LANDING GEAR CONTROL VALVE FROM FULLY RETURNING TO THE NORMAL POSITION. THE CABLE WAS REINSTALLED ON THE PULLEY AND THE LANDING GEAR WAS OPS CHECKED SEVERAL TIME WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: CONTROL CABLE — ICED UP (RT MLG WW)
KHA - FLT 805 - SFO-SEA - ON APPROACH TO SEA THE FLIGHT CREW FOUND THE LANDING GEAR HANDLE STUCK IN THE UP POSITION. THE CREW ELECTED TO USE ALTERNATE GEAR EXTENSION PROCEDURES AND MADE AN UNEVENTFUL LANDING. INSPECTION FOUND A BLOCK OF ICE HANGING ON THE LANDING GEAR CONTROL VALVE CABLES. THE ICE WAS REMOVED THE CABLE WERE LUBED AND A RETRACTION TEST WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BEAM — CRACKED (BS 178)
DURING INSPECTION FOR AD 81-10-10 A 1 INCH CRACK WAS FOUND ON THE NR 1 BEAM IN THE UPPER FORWARD CORNER OF THE FORWARD GALLEY SERVICE DOOR. THE BEAM WAS REPAIRED IAW THE DOUGLAS SRM CHAPTER 52 FIG 25. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 568 LBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (BS 568)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (FUSLAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 519 RBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (BS 519)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (BS 585)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: BLKHD T-CAP — CORRODED (WS 58.5)
DURING INSPECTION OF CORROSION TASK 13-57301 WHILE AIRCRAFT WAS IN C-CHECK LEVEL 2 CORROSION WAS FOUND ON THE SURFACE OF THE WING BULKHEAD LOWER T-CAP AT STATION 58.5 OF THE LEFT WING BETWEEN STRINGER 11 THROUGH 17. THE T-CAP WAS REPAIRED IAW WITH DC-9 SB 57-98 SB 57-98. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 675 RBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 634 LBL 44.5. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 428 LBL 44.5. (M)
Part: SEAT TRACK — MISREPAIRED (BS 764)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: TRACK — MISREPAIRED (BS 694)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 604 RBL 44.5. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 680 LBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (BS 571)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: TRACK — MISREPAIRED (BS 383)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 383 LBL 44.5. (M)
Part: SEAT TRACK — MISREPAIRED (BS 680)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 517 LBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (BS 604)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REFERENCE GAIA9815.
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 784 RBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 585 LBL 22. (M)
Part: CHANNEL — CORRODED (BS 776)
DURING INSPECTION OF CORROSION TASK 58-53301 WHILE AIRCRAFT WAS IN C-CHECK, LEVEL 2 CORROSION WAS FOUND ON A FLOOR CHANNEL AT FUSELAGE STATION 776 LBL 33. THE CHANNEL WAS REPAIRED IAW KITTY HAWK EA D9-53-051. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — MISREPAIRED (BS 695)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 695 LBL 44.5. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 674 RBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (BS 634)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 516 LBL 44.5. (M)
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 764 LBL 22. (M)
Part: SEAT TRACK — MISREPAIRED (BS 694)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REFERENCE GAIA9815.
Part: SEAT TRACK — MISREPAIRED (FUSELAGE)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 602 LBL 44.5. (M)
Part: SKIN — DENTED (BS 211)
DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR AND DENT ON THE FUSELAGE SKIN JUST BELOW THE FORWARD ENTRANCE DOOR BETWEEN LONGRON 20L AND 18L AT FUSELAGE STATION 211. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-049. (M)
Part: SEAT TRACK — MISREPAIRED (BS 784)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (BS 606)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (BS 516)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (BS 675)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SKIN — CRACKED (BS 817)
DURING INSPECTION OF THE FUSELAGE SKIN PER AD 81-26-03R1 SIX CRACKS WERE FOUND AT STATION 817. FOUR CRACKS BETWEEN L2R ANDL3R AND TWO CRACKS BETWEEN L1 AND L2L. THE SKIN WAS REPAIRED IAW SERVICE REWORK DRAWING J060143. (M)
Part: BLKHD T-CAP — CORRODED (WS 58.5)
DURING INSPECTION OF CORROSION TASK 14-57301 WHILE AIRCRAFT WAS IN C-CHECK LEVEL 2 CORROSION WAS FOUND ON THE SURFACE OF THE WING BULKHEAD LOWER T-CAP AT STATION 58.5 OF THE RIGHT WING BETWEEN STRINGERS 11 THROUGH 16. THE T-CAP WAS REPAIRED IAW THE DC-9 SB 57-98. THE A/C WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — MISREPAIRED (BS 695)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (BS 428)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: SEAT TRACK — MISREPAIRED (BS 602)
DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KITTY HAWK EA D9-53-051. REF GAIA9815.
Part: BUNGEE — LEAKING (RT MLG)
KHA - FLT 1563 - PIA-ELP - ON APPROACH TO ELP, THE FLIGHT CREW NOTICED THE LANDING GEAR WAS SLOW TO EXTEND. THE CREW ELECTED TO CYCLE THE GEAR AND NOTED THE SAME RESULTS. A UNEVENTFUL LANDING WAS MADE. THE AIRCRAFT WAS FERRIED GEAR DOWN TO DFW INVESTIGATION FOUND THE RIGHT MAIN LANDING GEAR BUNGEE CYLINDER LEAKING. THE BUNGEE CYLINDER WAS REPLACED AND THE LANDING GEAR WAS OPS CHECKED SEVERAL TIME WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
1996
Part: FRAME — CRACKED (CARGO COMPT)
DURING C-CHECK INSPECTION REVEALED 6 CRACKED STRUT FRAME ATTACH FITTINGS IN THE LOWER FUSELAGE CARGO COMPARTMENTS. CLOSER INSPECTION REVEALED THE CRACKS TO BE CORROSION CRACKS ALONG GRAIN LINES. FOUR FRAMES WERE REPLACED IAW THE DOUGLAS SRM AND TWO OF THE FRAMES WERE REPAIRED IAW KITTY HAWK E.A. D9-53-011. REF: STA 427, 680 BETWEEN L22L AND L25L. STA 387, 661, 680, 699 BETWEEN L22R AND L25R. (X)
1995
Part: DOWNLOCK SWITCH — ICED UP (LT MLG)
KHA - FLT 290 - TRI/ROC - ON APPROACH TO ROC, LT MLG DID NOT INDICATE DOWN AND LOCKED. GREEN LIGHT DID NOT ILLUMINATE. FLIGHT CREW DECLARED AN EMERGENCY, A NORMAL UNEVENTFUL LANDING WAS MADE IN ROC. ON TAXI TO RAMP, GROUND PERSONNEL NOTED LT INBOARD MAIN WHEEL WAS NOT ROTATING. MAINTENANCE FOUND LT DOWNLOCK SCISSOR LINKAGE ENCASED IN ICE, AND NR 2 MLG TIRE FLAT (FROM SKIDDING). THAWED SCISSOR LINKAGE AND CLEANED LT DOWNLOCK SWITCH CONNECTOR. DOWNLOCK INDICATION FUNCTIONALLY CHECKED NORMAL. REPLACED BOTH LT MLG WHEEL ASSEMBLIES. AIRCRAFT RELEASED FOR FLIGHT. (X)
Part: GEAR SELECTOR — MALFUNCTIONED (INST PANEL)
YIP/OKC - FLT 511 - DURING APPROACH TO OKC, FLIGHT CREW DISCOVERED LANDING GEAR SELECTOR WOULD NOT MOVE DOWN. ABNORMAL LANDING GEAR EXTENSION PROCEDURES WERE FOLLOWED AND THE GEAR WAS EXTENDED. PRIOR TO CROSSING THE OUTER MARKER, THE LANDING GEAR SELECTOR WAS TRIED AGAIN AND MOVED TO THE DOWN POSITION. AN UNEVENTFUL LANDING WAS MADE. THE LANDING GEAR SELECTOR WAS LUBRICATED AND A DRAIN LINE WAS REPOSITIONED, THE GEAR SELECTOR WAS OPERATED SEVERAL TIMES WITH NO BINDING. THE AIRCRAFT WAS NON-REVENUE FERRIED TO DFW AND A RETRACTION TEST WAS PERFORMED WITH NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. (X)