N633AS
Registered owner: CUSTOM DRONE SOLUTIONS INC, MN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Atlantic Southeast Airlines, Inc. | Operator | on 1994-12-12 | Operator named in NTSB report |
Accident & incident history
Operated by ATLANTIC SOUTHEAST AIRLINES (per NTSB report)
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.
94 reports on file, 1996-03-27 – 2008-06-23.
Part: HANDLE — MISINSTALLED (EMERGENCY EXIT) · airframe 32,208 hrs · 35,770 cycles
ROW 1D EMERGENCY EXIT HANDLE VERY HARD TO PULL. INSTALLED RT EMERGENCY HATCH CORRECTLY. OPS CHECK GOOD. (S)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,631 hrs · 35,171 cycles
ASD EMERGENCY LIGHT INOP.
Part: SKIN — CRACKED (RT WING) · airframe 31,409 hrs · 34,934 cycles
CRACK FOUND ON RIGHT WING LOWER SKIN AT RIB 19.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
INTERCOSTAL AND CHORD ANGLE CORRODED BETWEEN FR 38-39 STR 17L. INTERCOSTAL REPLACED IAW SRM 51-25-01.
Part: PANEL — CORRODED (PAX DOOR) · airframe 31,409 hrs · 34,934 cycles
PAX DOOR STAIRCASE, VERTICAL PANEL NR 1 FROM TOP, LIGHT DOUBLER CORRODED.
Part: ANGLE — CRACKED (LT WING) · airframe 31,409 hrs · 34,934 cycles
ON TOP OF LEFT WING BOX AT FR 23D AND RIB 1 ANGLE OF INTERCOSTAL FOUND CRACKED. FABRICATION OF ANGLE OF INTERCOSTAL ON LEFT WING BOX AT FR 23D RIB 1 COVERED ON W/C 2000-146. ANGLE OF INTERCOSTAL ON TOP OF LEFT WING BOX AT FR 23D RIB 1 INSTALLED IAW SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
RIGHT I/B SEAT TRACK BETWEEN FR 13 TO FR 17 FOUND CORRODED. RIGHT INBOARD SEAT TRACK BETWEEN FR 13 TO 17 CORROSION REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304. MATERIAL THICKNESS: 0.090 MATERIAL REMOVED: 0.010 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
RIGHT SEAT TRACK FOUND CORRODED BETWEEN FR 36-38. CORROSION REMOVED ON FLOORBEAM AT FR 36 AS PER SRM 51-21-42 & WITHIN LIMITS AS PER SRM 53-00-00 FIG 304. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 53-00-00 FIG 304. MATERIAL THICKNESS: 0.063, MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
RIGHT SEAT TRACK FOUND CORRODED BETWEEN FR 36-38. RIGHT SEAT TRACK CORROSION REMOVED BETWEEN FR 36-38 AS PER SRM 51-21-42 & WITHIN LIMITS AS PER SRM 53-00-00 FIG 304. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 53-00-00 FIG 304 SRM MATERIAL THICKNESS: 0.090 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
CORROSION FOUND ON LEFT SEAT TRACK BETWEEN FR 39 TO FR 41. CORROSION ON LEFT SEAT TRACK BETWEEN FR 39 TO 41 REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304. MATERIAL THICKNESS: 0.090, MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: BRACKET — BROKEN (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
OMEGA BRACKET & NUT PLATE BROKEN AT FR 39 BETWEEN STR LT 13 & 14.
Part: PLATE — CRACKED (RT WING) · airframe 31,409 hrs · 34,934 cycles
RIGHT WING BOX AT FR 28A FACE PLATE FOUND CRACKED. FACE PLATE AT FR 28A RIGHT WING BOX REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: ANGLE — CRACKED (RT MLG WW) · airframe 31,409 hrs · 34,934 cycles
RIGHT WHEEL WELL (MAIN) 2 ANGLES CRACKED AT FR 27 STR RT 17.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
RIGHT SEAT TRACK FOUND CORRODED BETWEEN FR 39 TO FR 41. RIGHT SEAT TRACK CORROSION REMOVED BETWEEN FR 39 TO FR 41 AS PER SRM 51-21-42 & WITHIN LIMIT AS PER SRM 53-00-00 FIG 304. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304, MATERIAL THICKNESS: 0.090, MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
INTERCOSTAL CRACKED IN LEFT MLG W/W AT FR 27.
Part: PANEL — CORRODED (PAX DOOR) · airframe 31,409 hrs · 34,934 cycles
PAX DOOR STAIRCASE, VERTICAL PANEL NR 1 FROM TOP, CORRODED UNDER LIGHT DOUBLER.
Part: ANGLE — CRACKED (RT WING) · airframe 31,409 hrs · 34,934 cycles
ON TOP OF RIGHT WING BOX AT FR 23D AND RIB 1 ANGLE OF INTERCOSTAL FOUND CRACKED. FABRICATION OF ANGLE OF INTERCOSTAL ON RIGHT WING BOX AT FR 23D RIB 1 COVERED ON W/C 2000-161. ANGLE OF INTERCOSTAL ON TOP OF RIGHT WING BOX FR 23D RIB 1 REPLACED AS PER SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
STR LEFT 17 + INTERCOSTAL CORRODED BETWEEN FR 36-38. CORROSION REMOVED ON STR LEFT 17, BETWEEN FR 36 & 38 + INTERCOSTAL AS PER SRM 51-21-42. U/T PERFORMED BY HEATHAIR AMO 46-90 W/O 38178 IAW NTM N=0.063" MIN=0.047" STR 17 LEFT WILL BE REPLACED ON W/C 100-65. MATERIAL THICKNESS: 0.063, MATERIAL REMOVED: 0.016 OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. SUPPLEMENTAL SDR CLOSED 1/15/08.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
STR LEFT 17 CORRODED BETWEEN FR 38-39. CORROSION REMOVED ON STRG L/H 17 BTW FR 38 & 39 AS PER SRM 51-21-42.
Part: STRUCTURE — CRACKED (RT WING) · airframe 31,409 hrs · 34,934 cycles
RIGHT WING BOX AT FR 28A FOUND CRACKED. FR 28A OF RIGHT WING BOX REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,409 hrs · 34,934 cycles
CORROSION FOUND ON LEFT SEAT TRACK BETWEEN FR 36 TO FR 39. CORROSION ON LEFT SEAT TRACK BETWEEN FR 36 TO 39 REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304. MATERIAL THICKNESS: 0.090, MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08.
Earlier reports · 1996–2007 · 73 reports
2007
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,363 hrs · 34,891 cycles
RIGHT SIDE FUSELAGE EMERGENCY LIGHT INOP.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,149 hrs · 34,671 cycles
TWO MINUTE LIGHTING WILL NOT SHUT OFF. FLT 4726 DEL 32 MINS.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 31,128 hrs · 34,655 cycles
FLAP ASYM AFTER TAKEOFF. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.
Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 31,093 hrs · 34,622 cycles
PASSENGER DOOR EMERGENCY LIGHT INOP.
Part: LIGHT — INTERMITTENT (CABIN) · airframe 31,072 hrs · 34,600 cycles
TWO MIN LIGHT COMES ON INTERMITTENT.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 31,027 hrs · 34,557 cycles
THE "TWO MINUTE" LIGHTS WILL NOT EXTINGUISH.
Part: HYDRAULIC SYSTEM — LOW · airframe 30,715 hrs · 34,255 cycles
AFTER TAKEOFF OUT OF ATL GOT A BLUE HYDRAULIC SYSTEM LOW LEVEL. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. FLT 4437 DEL 15 MINS. FLTS 4697, 4837(X2), 4181, 4624, 4536 CX.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,708 hrs · 34,246 cycles
ASD EMERGENCY LIGHT IS INOP.
Part: LIGHT — INOPERATIVE (ASD) · airframe 30,166 hrs · 33,644 cycles
EMERGENCY LIGHT OUT ON ASD.
Part: UNKNOWN — ODOR (CABIN) · airframe 29,919 hrs · 33,363 cycles
ON DESCENT UNUSUAL SMELL FROM VENTS, FLIGHT COMP TEMP (PACKS).
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,894 hrs · 33,331 cycles
RIGHT WING BOX DTW FR 244 24 INTERCOSTAL FOUND CRACKED. REPAIRED IAW SRM 51-25-01.
Part: PLATE — CRACKED (RT WING) · airframe 29,894 hrs · 33,331 cycles
RIGHT WING BOX AT FR 28 FACE PLATE CRACKED. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01
Part: ANGLE — CRACKED (WING BOX) · airframe 29,894 hrs · 33,331 cycles
RIGHT WING BOX AT FR 28 ANGLE BEHIND FACE PLACED CRACKED. NEW SHEETMETAL BENT INSTALLED IAW SRM 51-25-01 AT FR28 WING BOX. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SR663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.
Part: PLATE — CRACKED (FUSELAGE) · airframe 29,894 hrs · 33,331 cycles
LEFT WING BOX AT FR 28A FACE PLATE CRACKED. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP633 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01
Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,894 hrs · 33,331 cycles
LEFT WING BOX AT FR 28 ANGLE BEHIND FACE PLATE CRACKED. LT WING BOX AT FR28 ANGLE BEHIND FACE PLATE REPLACED PER SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW S.P. 663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01.
2006
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,606 hrs · 32,981 cycles
ASD EMERGENCY LIGHT INOP.
Part: LIGHT — INOPERATIVE (AIRSTAIR) · airframe 29,540 hrs · 32,904 cycles
ASD STEP LIGHT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,890 hrs · 32,127 cycles
FLOOR EMER LIGHT TRACK OUT AT ROWS 12,13, AND ROW 4.
Part: LIGHT — INOPERATIVE (AIRSTAIRS) · airframe 28,890 hrs · 32,127 cycles
ASD STEP LIGHT INOP.
Part: LIGHT — INOPERATIVE (AFT AIRSTAIRS) · airframe 28,794 hrs · 32,009 cycles
ASD STEP LIGHT INOP. (CLOSED)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,585 hrs · 31,732 cycles
ASD EMERGENCY LIGHT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,509 hrs · 31,627 cycles
ASD STEP LIGHT INOP.
Part: UNLOCK SWITCH — UNKNOWN (CABIN COOL SYS)
DURING CLIMB OUT, THE CREW DETECTED A BURNING RUBBER SMELL IN BOTH THE COCKPIT AND THE CABIN. THE CREW COMPLIED WITH THE AIR CONDITION SMOKE CHECKLIST AND THE SMELL SUBSIDED AFTER THE LT PACK WAS TURNED OFF. THE AIRCRAFT LANDED SAFELY. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF BOTH PACKS WITH BOTH ENGINES RUNNING WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: LAMP — BURNED OUT (EMERGENCY LIGHT)
DURING A HANGAR INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY LIGHT ASSY. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)
Part: SWITCH — BROKEN (EMERGENCY LIGHTS)
DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS REMAINED ON WHEN IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT TOGGLE SWITCH. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT TOGGLE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
2005
Part: LIGHT — MALFUNCTIONED (CABIN)
DURING A GROUND INSPECTION, THE BACK EMERGENCY LIGHTS STAY ON WHEN ARMED AND DURING TAXI. MAINTENANCE CYCLED THE EMERGENCY LIGHTS TOGGLE SWITCH IN THE ARMED POSITION WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: LAMP — BURNED OUT (EMERGENCY LIGHT)
DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LAMP — BURNED OUT (CABIN) · airframe 27,872 hrs
DURING A HANGAR INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: LIGHT — INOPERATIVE (PAX DOOR)
DURING A GROUND INSPECTION IN AGS, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE PASSENGER DOOR LIGHT SYSTEM IAW ATR-72 AMM 33-51-11 WITH THE EMERGENCY SWITCHES ON. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECK GOOD. (M)
Part: LAMP — BURNED OUT (EMERGENCY LIGHT)
DURING A GROUND INSPECTION IN ATL, THE EMERGENCY TRACK LIGHTS, NEAR SEATS 6A AND 6B WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY TRACK LIGHT LAMP, NEAR 6A AND 6B. OPERATIONAL CHECKS GOOD. (M)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ASSEMBLY ON THE PAX DOOR. OPERATIONAL CHECKS GOOD. (M)
Part: COVER — MISSING (EMERGENCY LIGHT)
DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHT COVER AT ROW 1-D WAS FOUND WITH THE WORK (EXIT) MISSING. MAINTENANCE REMOVE AND REPLACED THE EMERGENCY EXIT FLOOR LIGHT COVER AT ROW 1-D. (K)
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)
DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LAMP — LOOSE (EMERGENCY LIGHT)
FLT 4733 - DURING A GROUND INSPECTION IN PFN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESEATED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LAMP — BURNED OUT (EMERGENCY LIGHT)
DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (K)
Part: LAMP — BURNED OUT (EMERGENCY LIGHT)
DURING HANGAR MAINTENANCE IN MCN, THE AFT TWO MINUTE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT TWO MINUTE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: WEB — CRACKED (WING)
DURING A C-CHECK IN YUL, THE WEB IN WING BOX FRAME 28 RIGHT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE WEB IN THE WING BOX FRAME 28 RT IAW SRM 51-25-01. (M)
Part: STRUCTURE — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE OUTER CHORD AT FRAME 14 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTER CHORD AT FRAME 14 LEFT IAW SRM 51-25-04. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36 LEFT IAW SRM 51-25-04. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE INBOARD AND OUTBOARD SEAT TRACKS BETWEEN FRAME 28-29 RT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD SEAT TRACKS BETWEEN FRAME 28-29 RT IAW SRM 53-00-00 FIG 434. (M)
Part: STRINGER — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL THE FS 40, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 40, STRINGER 14R IAW SRM 51-25-01. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE INBOARD SEAT TRACKS BETWEEN FRAME 31-31 LEFT/RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD SEAT TRACKS BETWEEN FRAME 31-32 LT/RT IAW SRM 51-25-04. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE OUTBOARD SEAT TRACK BETWEEN FRAME 25-26 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SEAT TRACK BETWEEN FRAME 25-26 LEFT IAW SRM 51-25-04. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36, RBL 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SEAT TRACK BETWEEN FRAME 29-36, RBL 40 IAW SRM 51-25-04. (M)
Part: CREASE BEAM — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE CREASE BEAM BETWEEN FRAME 39-40 RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM BETWEEN FRAME 39-40 RT IAW SRM 51-25-01. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FRAME 36 AND 38 RT, STRINGER 16 AND 17 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FRAME 36/38, RT, STRINGER 16/17 IAW SRM 51-25-01. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FRAME 38-39 LEFT WAS FOUND TO BE CORRODED ON THE LOWER FLANGE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FRAME 38-39 LEFT IAW SRM 51-25-01. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE SEAT TRACK BETWEEN FRAME 41 AND 44 RT WAS FOUND TO BE CORRODED IN THE CROWN BETWEEN FRAME 41-42 BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 41 AND 44 RIGHT IAW SRM 51-25-04. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FRAME 38/40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 38/40 IAW SRM 51-25-01. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FRAME 36-38 LEFT WAS FOUND TO BE CORRODED ON THE UPPER AND LOWER FLANGE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL BETWEEN FRAME 36-38 LEFT IAW SRM 51-25-01. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE SEAT TRACK BETWEEN FRAME 39 AND 40 RIGHT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 39 AND 40 RT IAW SRM 51-25-04. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE SUPPORT PLATE BETWEEN FRAME 13-17 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SUPPORT PLATE BETWEEN FRAM 13-17 LEFT IAW SRM 53-31-00, 51-21-42 AND 51-25-01. (M)
Part: FRAME — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE FRAME 37 RT, STRINGER 14 ON THE AFT SIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FRAME 37 RT, STRINGER 14 IAW ASA EO 72-53-0162. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT BETWEEN FRAME 39 AND 41 IAW SRM 51-25-01. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE SEAT TRACKS BETWEEN FRAME 36 AND 39 LEFT/RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FRAME 36 AND 39 LT/RT IAW SRM 51-25-04. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FS 36, STRINGER 14L AND 14R AND FRAME 39, STRINGER 14L AND 14R WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 36, STRINGER 14L AND 14R IAW SRM 51-25-01. (M)
Part: CHANNEL — CORRODED (FUSELAGE)
DURING A C-CHECK IN YUL, THE FORWARD CARGO FLOOR DRAIN CHANNEL BETWEEN FRAME 13-17 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR ON THE FORWARD CARGO FLOOR DRAIN CHANNEL BETWEEN FRAME 13-17 LEFT IAW ASA EO 72-53-0161. (M)
Part: ANGLE — CRACKED (WINGBOX)
DURING A C-CHECK IN YUL, THE ANGLE IN THE WING BOX AT FS 28 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE IN THE WING BOX AT FS 28 RT IAW SRM 51-25-01. (M)
2004
Part: LIGHT — INOPERATIVE (FUSELAGE)
DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2003
Part: LAMP — INOPERATIVE (PAX DOOR)
DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
DURING A GROUND INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DURING AN 'A' CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: A/C PACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN BNA, THE RT SIDE C-CHECK CHANNEL AT THE SERVICE DOOR BETWEEN FRAMES 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE 'C' CHANNEL AT THE SERVICE DOOR BETWEEN FRAMES 38 AND 39 IAW SRM 51-24-01 AND 51-25-04. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A C-CHECK IN BNA, THE LEFT AND RIGHT SEAT TRACKS AT FRAMES 36 THROUGH 39, AND THE LEFT SEAT TRACK AT FRAMES 39 THROUGH 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS AT FRAMES 36 THROUGH 39, AND THE LEFT SEAT TRACK AT FRAMES 39 THROUGH 41 IAW SRM 51-25-00 AND 51-25-04. (M)
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
DURING AN 'A' CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2002
Part: SIGN — INOPERATIVE (CABIN)
DURING A HANGER INSPECTION, THE LT FORWARD LOWER EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE RT EXTERNAL EMERGENCY LIGHT AT THE SERVICE DOOR WAS ALSO FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE EMERGENCY EXIT SIGN ASSEMBLY AND THE EMERGENCY LIGHTING POWER SUPPLY AT ROW 11AB. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE.
2000
Part: VALVE — INOPERATIVE (A/C PACK)
FLT 4060 - ON CLIMB-OUT FROM CHA AROUND 1500 FEET, FLIGHT ATTENDANT CALLED COCKPIT AND REPORTED SMELLING SMOKE AND SEEING A HAZE IN THE CABIN. AIRCRAFT RETURNED TO CHA AND LANDED SAFELY. LOCAL MAINTENANCE GROUND RAN ENGINE. MAINTENANCE INSPECTIONS FOUND RIGHT PACK INOPERATIVE. REPLACED RIGHT PACK VALVE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
1997
Part: O-RINGS — CUT (LT PCU)
DURING CRUISE FLT TRI-ATL, LEFT ENGINE LOST OIL PRESSURE AT 12,000 FEET MSL. CCAS AND LOCAL ALERTS ACTIVATED. LEFT ENGINE WAS SHUT DOWN PER THE QRH, FLIGHT CONTROL AND MAINTENANCE CONTROL WERE NOTIFIED. AN EMERGENCY WAS DELCARED AND FLIGHT CONTINUED TO THE NEAREST SUITABLE AIRPORT (ATL) WHERE LANDING WAS MADE SAFELY WITHOUT FURTHER INCIDENT. ATL MAINTENANCE FOUND PCU TRANSFER TUBE O-RINGS CUT. REMOVED AND REPLACED LEFT PCU TRANSFER TUBE AND O-RINGS. OPERATIONAL AND LEAK CHECKS WERE GOOD IAW/MM. AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)
1996
Part: OIL PRESS TRANSM — INOPERATIVE (LT ENGINE)
OKC/DFW - ON APPROACH, THE LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED BRIEFLY AND CREW DECLARED AN EMERGENCY. THE CAPTAIN REDUCED POWER DUE TO TURBULENCE AND THE OIL PRESSURE STABILIZED FOR THE REST OF THE FLIGHT. CREW NOTIFIED THE TOWER THE ENGINE WAS NOT SHUT DOWN AND THAT EVERYTHING WAS NORMAL. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT AT DFW. REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE TRANSMITTER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. (X)