N844AS
Registered owner: AGRI SPRAY DRONES LLC, MO (owner ≠ operator)
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.
283 reports on file, 2002-01-18 – 2016-09-04.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,690 hrs · 35,663 cycles
LEFT EXIT ROW EMERGENCY EXIT MARKER INOPERATIVE. R & R LT EXIT ROW EMERGENCY EXIT MARKER IAW AMM 33-51-13. OPS CHECK GOOD. SDR CLOSED.
Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,156 hrs · 35,102 cycles
ROW 8A EMERGENCY EXIT,EXIT SIGN INOPERATIVE. R & R ROW 8A LIGHTED EXIT SIGN IAW AMM 33-51-10. OPS CHECK GOOD.
Part: DOOR — UNKNOWN (MAIN PAX) · airframe 37,894 hrs · 34,805 cycles
PAX DOOR WILL NOT LOCK IN CLOSED POSITION AND WILL NOT OPEN. C/W OPS TEST GOOD IAW AMM 52-11-02, NO DEFECT NOTED.
Part: DOOR — BINDING (MAIN PAX) · airframe 37,619 hrs · 34,496 cycles
PASSENGER DOOR WILL NOT OPEN FROM INSIDE. HAD TO GET RAMP TO OPEN FROM OUTSIDE. INSPECTED PASSENGER DOOR AND LATCH MECHANISM AND PAX DOOR HANDLE NO DEFECTS NOTED REF AMM 52-11-00.
Part: DOOR — BINDING (PAX DOOR) · airframe 37,619 hrs · 34,496 cycles
DOOR HANDLE STUCK COULD NOT OPEN DOOR FROM INSIDE MAIN DOOR. INSP DOOR NO DEFECT NOTED OPENED AND CLOSED DOOR IAW AMM 52-11-00 DOOR OPERATE NORMALLY. ACFT OK FOR SERVICE.
Part: LINKAGE — FOULED (PAX DOOR) · airframe 37,608 hrs · 34,481 cycles
MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. FOUND LANYARD CAUGHT UP IN LINKAGE. RESECURED LANYARD AND PERFORMED OPS TEST OF PASSENGER DOOR IAW AMM 52-11-00. OPS TESTED 10 TIMES. NO DEFECTS NOTED AT THIS TIME.
Part: DOOR — BINDING (MAIN PAX) · airframe 37,590 hrs · 34,459 cycles
MAIN PASSENGER DOOR WOOULD NOT OPEN FROM THE INSIDE. PERFORMED OPS TEST OF PASSENGER DOOR SEVERAL TIMES IAW AMM 52-11-00. FURTHER FAULTS FOUND AT THIS TIME, OK FOR SERVICE.
Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 37,496 hrs · 34,359 cycles
CORROSION ON FWD SUPPORT ANGLE OF FLOOR PANEL 221ALF. BLENDED AND REMOVED CORROSION IAW SRM 51-21-06-00. RECEIVED AND COMPLIED WITH EA 15-2016-002.
Part: ATTACH ANGLE — CRACKED (BS 280-295) · airframe 37,496 hrs · 34,359 cycles
INBD AND OTBD ANGLES ATTACHED TO STR3L BETWEEN FS 280 TO FS 295 ARE CRACKED. REMOVED INBD AND OTBD ANGLE AT STR 3L BETWEEN FS 280 AND FS 294 IAW SRM 51-42-06. LOCATED TRANSFERED DRILLED MOUNT HOLES AND INSTALLED SERVICABLE INBD AND ON ANGLES AT STR 3L BETWEEN FS 280-FS 295 REF SRM 51-40-11, SRM 51-42-06 AND DWG 600-31057.
Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 37,496 hrs · 34,359 cycles
LT SIDE INTERCOSTAL CRACKED AT WL 80.00 BETWEEN FS 621.00 AND 625.30. REMOVED CRACKED INTERCOSTAL AT WS 80.00 BETWEEN FS 621.00 AND 625.30 THEN INSTALL NEW INTERCOSTAL AT SAME LOCATION IAW SRM 51-42-06, 51-42-21.
Part: BRACKET — CRACKED (BS 640) · airframe 37,496 hrs · 34,359 cycles
AFT EQUIPMENT SUPPORT STRUCTURE RT FWD POST TIE PLATE CRACKED, FS 640.00 STR 24RH. REMOVED CRACKED BRACKET, INSTALLED NEW BRACKET AT AFT EQUIPMENT BY APU SUPPORT, RT AND LT FWD POST UPPER IB GUIDE IAW SRM 51-42-13.
Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 37,496 hrs · 34,359 cycles
LEFT SIDE INTERCOSTAL CRACKED AT WL 90.00 BETWEEN FS 621.00 AND FS 625.30. REMOVED INTERCOSTAL LT SIDE & STIFFENER FORM WL 90.00 BTS. FS 621 & 625 REF SRM 42-21 & SRM 51-42-00. LOCATED AND DRILLED LT SIDE INTERCOSTAL AT WL 90.00 BTS FS 621 AND FS 625.30 IAW SRM 51-40-11. INSTALLED INTERCOSTAL & STIFFENER AT SL 90.00 BTS FS 621 & 625.30 REF SRM 51-42-21 & SRM 51-42-06.
Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 37,496 hrs · 34,359 cycles
LT SIDE INTERCOSTAL CRACKED AT WL 84.00 BETWEEN FS 621.00 AND FS 625.30. R & R INTERCOSTAL AT WL 84, BS 621 IAW SRM 51-42-21, 51-42-02.
Part: ANGLE — CRACKED (BS 621-625) · airframe 37,496 hrs · 34,359 cycles
CLIP CRACKED AT WL 80.00 LT SIDE BETWEEN FS 621.00 AND 625.30. REMOVED CLIP AND WL 80 LT SIDE & REPLACED WITH SERVICEABLE CLIP WL80 BETWEEN FS 621 & FS 625.30 REF SRM 51-42-21.
Part: INTERCOSTAL — CRACKED (BS 621-525) · airframe 37,496 hrs · 34,359 cycles
LT SIDE INTERCOSTAL CRACKED AT WL 76.00 BETWEEN FS 621.00 AND 625.30. REMOVED CRACKED BRACKET, INSTALLED NEW BRACKET AT AFT EQUIPMENT BY APU SUPPORT, RT AND LT FWD POST UPPER INBD GUIDE IAW SRM 51-42-13.
Part: ANGLE — CRACKED (BS 621-625) · airframe 37,496 hrs · 34,359 cycles
CLIP CRACKED AT WL 80.00 RT SIDE BETWEEN FS 621.00 AND 625.30. REMOVED CLIP AT WL 80 RT SIDE AND REPLACED WITH SERVICEABLE CLIP WL 80 BETWEEN FS 621 & FS 625.30 REF SRM 51-42-21.
Part: BRACKET — CRACKED (BS 280) · airframe 37,496 hrs · 34,359 cycles
CRACKED BRACKETS FOUND ON RBL9 AND 280 CROSSBEAM, BOTH OTBD & INBD CLIP. REMOVED 2 EA L-ANGLE CLIPS AT FS 280, RBL 9 OTBD ABD INBD IAW COMPLY WITH REO 601R-53-11. INSTALLED NEW L-ANGLE CLIP AT FS 280, RBL9 RT INBD IAW SRM 51-42-21. COMPLIED WITH REO 601R-53-11-2849. RECEIVED AND COMPLIED WITH ECTC REO601R-53-11-2849.
Part: BULKHEAD — CRACKED (BS 621) · airframe 37,496 hrs · 34,359 cycles
REAR PRESSURE BULKHEAD FORWARD FACE ABOVE FLOOR IS CRACKED AT BL 0.00 BETWEEN WL 73.50 AND WL 120.43. COMPLIED WITH ECTC REO601R-53-61-1285 08 AND GREO 601R-53-61-1285, REV D DATED: 10/31/2011 AS WRITTEN.
Part: ANGLE — CRACKED (BS 280) · airframe 37,496 hrs · 34,359 cycles
ASD UPPER FWD SILL CLIP CRACKED AT FS 280.00 AND STR 3. REMOVED CLEAT AT FS 280.00 AND STR 3 IAW SRM 51-42-06. LOCATED, TRANSFERD DRILLED MOUNTING HOLES AND INSTALLED SERVICEABLE CLEAT AT ASD UPPER SILL FWD AT FS 280 AND STR 3 REF SRM 51-40-11 AND SRM 51-42-06, REF DWG 604-34017.
Part: BRACKET — CRACKED (BS 280) · airframe 37,496 hrs · 34,359 cycles
CRACKED BRACKETS FOUND ON LBL9 AND 280 CROSSBEAM, BOTH OTBD AND INBD CLIP. REMOVED 2 EA, L-ANGLE CLIPS AT FS280, LBL9, OTBD ABD INBD IAW COMPLY WITH REO 601R-53-11. COMPLIED WITH REO 601R-53-11. RECEIVED AND COMPLIED WITH ECTC REO601R-53-11-2849.
Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 37,496 hrs · 34,359 cycles
CORROSION FOUND ON RT FLOOR SILL BETWEEN FS559.00-559.00+16. REMOVED CORROSION IAW SRM 51-21-06, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-01. REMOVED INTERCOSTAL FOR REPLACMENT. DRILLED UP NEW INTERCOSTAL. REF: SRM 51-42-06 AND 51-40-11. DWG: 601R38842, REV B. INSTALLED RT FLOOR SILL NEW SERIVCABLE AT FS559.00-559.00+16 IAW DWG 601R38842 AND SRM 51-42-06-00 AND 51-42-21-00 AND 51-41-00-00.
Part: STRUCTURE — CORRODED (BS 559) · airframe 37,496 hrs · 34,359 cycles
CORROSION ON SILL & AROUND HEATER VENT AT FS 559.00 -559.00+80, RBL 40-45. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 37,496 hrs · 34,359 cycles
CORROSION FOUND ON SEAT RAIL AT FS 559.00+80 & RBL 9. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. R & R SEAT RAILS AT FS 559.00 TO 559.00+80, RBL 9 IAW SRM 51-41-00-00 51-41-04 & IAW AMM 53-01-11-000-802/400-802.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 37,496 hrs · 34,359 cycles
CORROSION FOUND SEAT RAIL AT FS 559.00+80-559.00+96 AND RBL 27. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. R & R SEAT RAILS AT FS 559.00+80 TO +96 RBL27 IAW SRM 51-41-00-00 & 51-41-04 & AMM 53-01-11-000-802 & 53-01-11-400-802.
Part: FRAME — CRACKED (BS 621) · airframe 37,496 hrs · 34,359 cycles
CRACK FOUND AT 621.00 AND LBL 40. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-61-5619, REV O, DATED 2016-01-10. REMOVED 2 EA INTERCOSTALS TO GAIN ACCESS TO REPAIR AREA IAW SRM 51-42-21 AND 51-42-00. INSTALLED 2 EA INTERCOSTALS BACK TO ORIGINAL LOCATION IAW SRM 51-42-21, 51-42-06.
Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 37,496 hrs · 34,359 cycles
CORROSION FOUND BETWEEN BS 621 - 605 AND LBL 27. AREA IS OUT OF LIMIT IAW RED 601R-53-00-005, REV B. DATED JAN. 6, 2011, FIGURE 2. PERFORMED EDDY CURRENT INSPECTION IAW SRM 51-12-00, IAW 51-20-06. NO INDICATIONS NOTED AT THIS TIME. EVALUATED BLEND AT LBL 27 BETWEEN FS 621-605 FLOORBEAM AND FOUND IT TO BE OUT OF THE ALLOWABLE DAMAGE LIMITS R60-601R-53-00-005, FIG 2. REMOVED FLOORBEAM UPPER CAP BETWEEN FS 569 AND FS 621 AT LBL 27. REF SRM 51-42-021 AND 51-42-22. DRILLED UP NEW FLOORBEAM CAP REF SRM 51-40-11.
Part: PLATE — CRACKED (BS 589) · airframe 37,496 hrs · 34,359 cycles
CRACK FOUND ON SILL PLATE AT FS 589.00 & LBL40. COMPLIED WITH ECTC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B DATED 10/09/2009 AS WRITTEN.
Part: DOOR SILL — CORRODED (BS 559) · airframe 37,496 hrs · 34,359 cycles
CORROSION FOUND ON FLOOR SILL AT FS 559.00+80-559.00+12 AND LBL 40. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV DATED: 05/26/2013 AS WRITTEN.
Part: DOOR SILL — CORRODED (BS 574-621) · airframe 37,496 hrs · 34,359 cycles
CORROSION FOUND ON CARGO DOOR SILL AT 574.00- 621.00 AROUND SCREW HOLES LBL40-45 TO 27 . COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV DATED: 05/22/2013 AS WRITTEN.
Part: STRUCTURE — CORRODED (BS 559) · airframe 37,496 hrs · 34,359 cycles
CORROSION ON SILL AT AT FS 559.00-FS 559.00-559+32 LBL 40. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526.
Earlier reports · 2002–2015 · 253 reports
2015
Part: FAN — FAILED · airframe 37,442 hrs · 34,292 cycles
STRONG ELECTRICAL SMELL IN FLIGHT DECK. C/W OPS CHECK FOR STRONG ELECTRICAL SMELL IN FLIGHT DECK IAW AMM 21-24-19. OPS CHECK OK. DEFECT CLEARED. PLACARD REMOVED. ACFT OK FOR SERVICE. R & R OF GALLEY EXHAUST FAN.
Part: LIGHT — INOPERATIVE (ROW 8 AB) · airframe 36,446 hrs · 33,196 cycles
ROW 8 A/B FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-10. OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 35,780 hrs · 32,506 cycles
F/A FLASHLIGHT IS INOPERATIVE. R & R BATTERIES. OPS CHECKED GOOD IAW AMM 25-60-00. ACFT OK FOR SERVICE.
2014
Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 35,270 hrs · 31,995 cycles
FS 621 BULKHEAD, ISOLATORS ARE CRACKED. REMOVED AND REPLACED WITH NEW IAW SRM 51-42-06.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,270 hrs · 31,995 cycles
LT EMERGENCY EXIT MARKER LIGHTS ON WALL JUST FWD OF DOOR IS INOPERATIVE. REMOVED LT EMERGENCY EXIT MARKER IAW AMM 33-51-10-000-801. INSTALLED SERVICEABLE EMERGENCY EXIT MARKER IAW 33-51-10-400-801, PN 6020-6. OPS TEST ID GOOD.
Part: LIGHT — INTERMITTENT (CABIN) · airframe 34,910 hrs · 31,650 cycles
EMERGENCY LIGHT INOPERATIVE. PERFORMED OPS CHECK OF SIDEWALL EMERGENCY LIGHT IAW AMM 33-51-01.
Part: LIGHT — INTERMITTENT (CABIN) · airframe 34,910 hrs · 31,650 cycles
ONE EMERGENCY LIGHT INOPERATIVE. CABIN EMERGENCY LIGHTS ILLUMINATED. PERFORMED OPS CHECK OF SIDEWALL EMERGENCY LIGHT IAW AMM 33-51-01 DEFER CLEARED PLACARD REMOVED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,479 hrs · 31,245 cycles
CEILING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.
Part: SIGN — INOPERATIVE (CABIN) · airframe 34,402 hrs · 31,164 cycles
LEFT OVERWING EMERGENCY EXIT MARKER INOPERATIVE. R & R LT OVERWING EMERGENCY EXIT MARKER IAW AMM 33-51-10. OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,100 hrs · 30,882 cycles
LOWER EMERGENCY EXIT LIGHT AT SEAT 8A INOPERATIVE. PERFORMED OPS TEST OF THE EMERGENCY EXIT LIGHT AT SEAT 8A IAW AMM 33-51-00. NO DEFECTS NOTED AT THIS TIME.
Part: TRUNNION — DAMAGED (MLG) · airframe 33,770 hrs · 30,537 cycles
ONE HOLE AT LT FWD SIDE OF MLG TRUNNION STRAP NO GO SIDE OF COMBINATION GAGE GOES IN HOLE. REPAIRED IAW REO 601R-57-21-2087, REV P1. MAJOR REPAIR.
Part: TRUNNION — DAMAGED (MLG) · airframe 33,770 hrs · 30,537 cycles
ONE HOLE AT RT FWD SIDE OF MLG TRUNNION STRAP NO GO SIDE OF COMBINATION GAGE GOES IN HOLE. REPAIRED IAW REO 601R-57-21-2087, REV P1. MAJOR REPAIR.
Part: SKIN — CORRODED (LT WING) · airframe 33,770 hrs · 30,537 cycles
LT WING LOWER PLANK ACCESS HOLE FUEL PANEL 540BB HAS CORROSION. COMPLIED WITH REO 601R-57-21-030. MAJOR REPAIR.
Part: SKIN — CORRODED (RT WING) · airframe 33,770 hrs · 30,537 cycles
RT WING LOWER PLANK ACCESS HOLE FUEL PANEL 640BB HAS CORROSION. REPAIRED IAW REO 601R-57-21-030. MAJOR REPAIR.
Part: BULKHEAD — CRACKED (AFT) · airframe 33,770 hrs · 30,537 cycles
REAR PRESSURE BULKHEAD WEB FORWARD FACE IS CRACKED IN 2 PLACED AT RBL 27.50 BETWEEN WL 73.50 AND WL 120.43 AREAS ARE MARKED. COMPLIED WITH REO 601R-53-61-1285, REV D. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 529-544) · airframe 33,770 hrs · 30,537 cycles
RIGHT SIDE SEAT TRACK HAS CORROSION BETWEEN BS 529-544. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 33,770 hrs · 30,537 cycles
SEAT TRACK AT LBL 9 BETWEEN FS 394 - 409+128 HAS NUMEROUS PLACES OF CORROSION. R & R SEAT TRACK IAW REO 601R-53-00-485 STEPS 1-3.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,770 hrs · 30,537 cycles
RT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 559+16 - FS 559+32. REMOVED AND INSTALLED NEW SEAT TRACK BS 495.98 - 535.02, IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 33,770 hrs · 30,537 cycles
CARGO BAY HAS FOUR CARGO TRACKS AND ONE TIE DOWN CORRODED RBL 9.0. REMOVED AND REPLACED CARGO TRACKS IAW REO 601R-53-00-485. REMOVED AND REPLACED CARGO NET CLEAT IAW SRM 51-41-02-00.
Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,770 hrs · 30,537 cycles
SEAT TRACK AT LBL 9 CORRODED AFT OF BS 559+32. R & R SEAT TRACK IAW REO 601R-53-00-485.
Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 33,770 hrs · 30,537 cycles
SEAT TRACK AT RBL 9 BETWEEN BS 394-409+128 HAS NUMEROUS PLACES OF CORROSION. R & R SEAT TRACK IAW REO 601R-53-00-485 UP TO STEP 6
Part: HINGE — GOUGED (PAX DOOR) · airframe 33,770 hrs · 30,537 cycles
ASD HINGE GOUGED ON AFT AND ON AIRFRAME SIDE. COMPLIED WITH REO 601R-53-21-814. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 33,770 hrs · 30,537 cycles
RT SIDE FLOOR SUPPORT CORRODED ON TOP AND BOTTOM AT NUTPLATE HOLES BETWEEN BS 589-605. REPAIRED IAW REO 601R-53-61-5153, REV. MAJOR REPAIR.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,770 hrs · 30,537 cycles
ASD AFT ANGLE CRACKED. COMPLIED WITH REF 601R-52-11-513. COMPLIED WITH EC/TC REO 601R-52-11-513.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 33,770 hrs · 30,537 cycles
TWO SUPPORT BRACKETS CRACKED ON EMERGERCY EXIT FWD RT INTERNAL STRUCTURE. REMOVED SUPPORT BRACKET ON CREW ESCAPE HATCH IAW SRM 51-42-06 AND 57-42-13. INSTALLED NEW SERVICEABLE STOP SUPPORT FITTING ON CREW ESCAPE HATCH IAW SRM 51-42-06 AND 51-42-13 AND DWG 600-33243. MAJOR REPAIR.
Part: RIB — CRACKED (LT WING) · airframe 33,770 hrs · 30,537 cycles
LEFT MLG WHEEL WELL BATTERY RIB CRACKED. COMPLIED WITH REO 601R-57-51-046. COMPLIED WITH REO 601R-57-51-016. RECEIVED AND COMPLIED WITH EC/TC REO 601R-57-51-046 AS WRITTEN.
Part: ATTACH FITTING — GOUGED (PAX DOOR) · airframe 33,754 hrs · 30,520 cycles
FOUR GOUGED LUGS IN PAX DOOR HINGE. COMPLIED WITH REO 601R-52-11-1347 AND ECTC REO 601R-52-11-1347. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW IAW SOP 5702.
Part: SHROUD — GOUGED (RT AILERON) · airframe 33,770 hrs · 30,537 cycles
RIGHT AILERON OTBD L/E HAS A GOUGE. R & R RT AILERON L/E SHROUD IAW SRM 51-42-06 AND DWG 601R13031-166. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,770 hrs · 30,537 cycles
BRACKET AT FAIRING 161EL IS CRACKED. R & R BRACKET IAW SRM 51-42-06-00 AND SRM 51-42-15-00 IAW DWG 601R31037.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 33,770 hrs · 30,537 cycles
BRACKET FOR FAIRING 162DL IS CRACKED. REMOVED CRACKED BRACKET IAW SRM 51-42-06, PG 11. INSTALLED BRACKET IAW SRM 51-42-06 AND 51-42-10 AND DWG 601R31037-48.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,770 hrs · 30,537 cycles
DOOR EXIT SIGN BETA LIGHTS FAILED FUNCTIONAL TEST ON PAX DOOR, SERVICE DOOR, LT OVERWING EMERGENCY EXIT DOOR AND RT OVERWING EXIT DOOR. INSTALLED PAX DOOR AND SERVICE DOOR BETA LIGHTS IAW AMM 33-51-09, TASK 33-51-09-400-801. R & R BETA LIGHTS ON LT AND RT OVERWING EMERGENCY EXIT DOORS BY REMOVING 2 SCREW AND SELF-LOCKING NUTS AND INSTALLING 2 SCREWS AND SELF-LOCKING. R & R PAX DOOR BETA LIGHT IAW AMM 33-51-06-400-801. IPC LIGHT INTENSITY CHECKED GOOD. PERFORMED FUNCTIONAL TEST OF BETA LIGHTS IAW AMM 33-51-09-720-801. FUNCTIONAL TEST GOOD.
2013
Part: WARNING MESSAGE — ILLUMINATED (EXTINGUISHER) · airframe 33,714 hrs · 30,483 cycles
CARGO BOTTLE LOW CAUTION MESSAGE IN FLIGHT. ACFT DIVERTED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,658 hrs · 30,424 cycles
AFT LEFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW AMM 33-51-00.
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 32,752 hrs · 29,509 cycles
COVER ON EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR FALLING OFF. REPLACED EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-19, OPS CHECKS OK.
2012
Part: LANYARD — OUT OF POSITION · airframe 31,143 hrs · 27,875 cycles
PAX DOOR WOULD NOT OPEN FROM OUTSIDE. CLEARED DOOR RAIL LANYARD FROM RAILING. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECK OK AT THIS TIME. SDR CLOSED.
Part: PLACARD — PEELING (CABIN) · airframe 29,859 hrs · 26,467 cycles
EMERGENCY EXIT ARROW PLACARD, PASSENGER DOOR, PEALING OFF. R & R PLACARD IAW AMM 11-30-00.
Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,680 hrs · 26,268 cycles
EMERGENCY EXIT LIGHTED PLACARD FORWARD OF SERVICE DOOR INOPERATIVE. R & R PLACARD WITH SERVICEABLE UNIT IAW AMM 33-51-00-710-804 & 25-31-01-400-802. OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,674 hrs · 26,262 cycles
EMERGENCY LIGHTS ARE INOPERATIVE AT EMERGENCY EXIT DOORS. R & R NR 4 EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-04-400-801. OPS CHECKED GOOD IAW AMM 33-51-04-710-801.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,674 hrs · 26,262 cycles
EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-04-400-801. OPS CHECKED GOOD IAW AMM 33-51-04-710-801.
Part: THRESHOLD — CORRODED (BS 319.7-349) · airframe 29,669 hrs · 26,256 cycles
SERVICE DOOR SILL IS CORRODED FROM FS 319.70 -349.00. REPAIRED IAW AMM 51-23-00 AND SRM 51-25-06.
Part: FRAME — CORRODED (BS 333) · airframe 29,669 hrs · 26,256 cycles
GROUND WIRE STUD AT FS 333, STGR 26R HAS CORROSION. INSTALLED FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21.
Part: ANGLE — CORRODED (THRESHOLD) · airframe 29,669 hrs · 26,256 cycles
SERVICE DOOR THRESHOLD LOWER ANGLE FWD AND AFT ATTACH ANGLE CORRODED. BLENDED AFT ANGLE AND FOUND OUT OF LIMITS IAW SRM 51-21-06 AND SRM 53-00-00. REPLACED FWD ANGLE IAW SRM 51-42-06.
2011
Part: SILL — CORRODED (BS 349-369) · airframe 29,668 hrs · 26,254 cycles
RIGHT FLOOR SILL CORRODED FROM FS 349.00 - 369.00. REMOVED AND INSTALLED SILL IAW SRM 51-42-06 AND 51-42-21 AND EC/TC, REO 601R-53-21-326.
Part: SKIN — DENTED (RT WING) · airframe 29,669 hrs · 26,256 cycles
DENT FOUND ON RT WING AT WS 252.8 L/E 4.3750" X 1.5"W .040 DEEP FOUND ON WALK AROUND . REPAIRED IAW REO 601R-57-41-797.
Part: INTERCOSTAL — CORRODED (BS 349) · airframe 29,668 hrs · 26,254 cycles
INTERCOSTAL FS 349.00 CORRODED. REMOVED LIGHT SURFACE CORROSION FROM INTERCOSTAL IAW SRM 51-21-06. REPAIR IS CLASSIFIED AS MINOR.
Part: FRAME — CORRODED (BS 349) · airframe 29,668 hrs · 26,254 cycles
FRAME FS 349 CORRODED BETWEEN S24L TO 24R. REMOVED CORROSION.
Part: FRAME — CORRODED (BS 364) · airframe 29,668 hrs · 26,254 cycles
FRAME FS 364.00, CORRODED FWD SIDE BEWTEEN ST 26L AND 26R. REMOVED CORROSION FROM FRAME IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 51-21-06. APPLIED ALODINE, PRIMER & TOP COAT IAW SRM 51-21-11.
Part: RIB — CRACKED (LT NACELLE) · airframe 29,668 hrs · 26,254 cycles
RIB CRACKED BESIDE NUTPLATE FOR LT PYLON ACCESS PANEL 412AB. REPAIRED IAW REO 601R-54-61-073.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,668 hrs · 26,254 cycles
ANGLE CRACKED, FS 280, LBL 9 INBD SIDE OF FLOORBEAM. REMOVED CRACKED ANGLE IAW SEM 51-42-20. FABRICATED NEW ANGLE IAW REO 601R-53-11-171, ITEM 8. NDT TO ENSURE CLIP CRACK FREE. COMPLIED WITH STEP 8B OF EC/TC REO 601R-53-11-171 IAW NDTM PART 1, 51-20-08. NO INDICATIONS NOTED.
Part: ATTACH FITTING — CRACKED (BULKHEAD) · airframe 29,668 hrs · 26,254 cycles
ATTACH FITTING ON RT SIDE OF AFT REAR PRESSURE BULKHEAD AT APPROX 3 O'CLOCK POSITION IS CRACKED. DRILLED NEW ATTACH FITTING IAW SRM 51-40-11. INSTALLED ATTACH FITTING IAW SRM 51-42-21. REPAIR IS CLASSIFIED AS MAJOR.
Part: RIB — CRACKED (LT WING TE FLAP) · airframe 29,668 hrs · 26,254 cycles
LEFT OTBD FLAP INBD CLOSING RIB HAS A CRACK NEAR T/E. REMOVED AND REPLACED FLAP IAW AMM 27-54-05-400-801.
Part: SUPPORT — CORRODED (WINDSCREEN) · airframe 29,668 hrs · 26,254 cycles
RT WINDSCREEN SUPPORT CORRODED. FOUND OUT OF LIMITS & BEYOND 30 PERCENT OF SUFACE. DRILLED NEW WINDSCREEN SUPPORT TO FIT SURROUNDING STRUCTURE IAW SRM 51-40-11. INSTALLED WINDSCREEN SUPPORT BRACKET IAW SRM 51-42-06, 51-42-21 AND 51-42-13. REPAIR IS CLASSIFIED AS MINOR.
Part: SUPPORT — CORRODED (THRESHOLD) · airframe 29,668 hrs · 26,254 cycles
SERVICE DOOR THRESHOLD, CENTER SUPPORT CORRODED. CORROSION IS BEYOND 10 PERCENT THICKNESS. REPLACED SUPPORT IAW SRM 51-42-21. REPAIR IS CLASSIFIED AS MINOR.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,668 hrs · 26,254 cycles
SEAT TRACK CORRODED BETWEEN FLOOR PANELS 281KLF & 281ELF. CLEANED CORROSION FROM SEAT TRACK MAX MATERIAL LOSS AT 0.0215 MAX ALLOWABLE IS 0.020. OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK IAW AMM 53-01-11-04. REPAIR IS CLASSIFIED AS MAJOR.
Part: FITTING — CORRODED (BS 319.7) · airframe 29,668 hrs · 26,254 cycles
FITTING CORRODED AT FS 349 ON UPPER FRAME LEG AT FLOOR LEVEL. REMOVED AND INSTALLED FITTING IAW SRM 51-42-21. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,668 hrs · 26,254 cycles
CABIN FLOOR SUPPORT HAS CORROSION AT FLOOR PANEL. REMOVED FLOOR SUPPORT IAW SRM 51-42-06, CORROSION EXCEEDS ALLOWABLE DAMAGE IAW SRM 53-00-00. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-20-11 & 51-42-06. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
Part: BEAM — CORRODED (BS 349) · airframe 29,668 hrs · 26,254 cycles
TRANSVERSE BEAM FS 349 AND RBL 45 CORRODED ON TOP LEG OF BEAM. REMOVED AND REPLACED IAW SRM 51-42-06 AND SRM 51-42-21.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 29,668 hrs · 26,254 cycles
CAPTAIN'S LEFT SEAT TRACK IS WORN. CHECK LIMITS IAW SRM 53-11-49, FIG 101, SHT 2. FOUND TO BE OUT OF LIMITS MORE THAN 10 PERCENT MATERIAL LOSS, IAW SRM 53-11-49, FIG 101, SHT 2. REMOVED PILOTS OTBD SEAT TRACK ALL WORK DONE IAW AMM 53-01-01-000-801. LOCATED HOLES IN NEW SEAT TRACK ALL WORK DONE IAW SRM 51-41-02. INSTALL NEW SEAT TRACK. OK TO INSTALL TRACK MAC3QC 12/22/11. INSTALLED NEW CAPTAINS OTBD SEAT TRACK ALL WORK DONE IAW AMM 53-01-05-400-801. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA 5702. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REQUIRES 318 FORM TO BE FILLED OUT. COMPLETED M-318 AND FAXED TECH SUPPORT. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)
Part: FLOOR SUPPORT — CORRODED (BS 319.7) · airframe 29,668 hrs · 26,254 cycles
FLOOR SUPPORT AT FS 319.70, RBL 45 LOWER FWD CORNER OF SERVICE DOOR SURROUND CORRODED. REMOVED AND INSTALLED REF SRM 51-40-11 AND SRM 51-42-21. REPAIR IS CLASSIFIED AS MAJOR.
Part: DOUBLER — CORRODED (BS 320-348) · airframe 29,668 hrs · 26,254 cycles
DOUBLER ON INBD SIDE OF SERVICE DOOR THRESHOLD HAS CORROSION AT FWD & AFT CORNERS OF DOOR SURROUND AT FS 320 & 348. REMOVED AND INSTALLED DOUBLER IAW SRM 51-42-06. REQUIRES SDR.
Part: FITTING — CORRODED (BS 319.7) · airframe 29,668 hrs · 26,254 cycles
FITTING CORRODED AT FS 319.70 ON UPPER FRAME LEG AT FLOOR LEVEL. REMOVED AND REPLACED FITTING IAW SRM 51-42-21.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 29,668 hrs · 26,254 cycles
COPILOTS LEFT SEAT TRACK IS WORN. CHECK LIMITS IAW SRM 53-11-49. FOUND TO BE OUT OF LIMITS MORE THAN 10 PERCENT MATERIAL LOSS, IAW SRM 53-11-49, FIG 101, SHT 2. REMOVED CO-PILOTS INBD SEAT TRACK ALL WORK DONE IAW AMM 53-01-01-000-801. LOCATED HOLES IN NEW SEAT TRACK ALL WORK DONE IAW SRM 51-41-02. INSTALL NEW SEAT TRACK. OK TO INSTALL TRACK. INSTALLED CO-PILOTS INBD SEAT TRACK (NEW) ALL WORK DONE IAW AMM 53-01-05-400-801. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA 5702. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REQUIRES 318 FORM TO BE FILLED OUT. COMPLETED M-318 AND FAXED TECH SUPPORT. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)
Part: SILL — CORRODED (BS 310-319) · airframe 29,668 hrs · 26,254 cycles
RIGHT FLOOR SILL FS 310-319 CORRODED RBL45. REMOVED SECTION OF RT FLOOR SILL FROM FS 310 -319 BLENDED DAMAGE ORIGINAL MATERIAL .063 REMAINING MATERIAL .041 REF SRM 51-21-06. DAMAGE FOUND OUT OF LIMITS REF SRM 53-00-00. INSTALLED NEW SILL SECTION & NEW SILL DOUBLER IAW SRM 51-42-06.
Part: FLOOR SUPPORT — CORRODED (BS 319.7) · airframe 29,668 hrs · 26,254 cycles
FLOOR SUPPORT ANGLE AT THE SERVICE DOOR IS CORRODED ON THE UNDERSIDE AT FS 319.70. SUPPORT ANGLE WAS R & R.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,668 hrs · 26,254 cycles
SEAT TRACK CORRODED BETWEEN FLOOR PANELS 281DLF AND 281JLF. CLEANED CORROSION FROM SEAT TRACK, MAX MATERIAL LOSS AT 0.0215, MAX ALLOWABLE IS 0.020. FOUND OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK IAW AMM 53-01-11-04. REPAIR IS CLASSIFIED AS MAJOR.
Part: SILL — CORRODED (BS 559) · airframe 29,668 hrs · 26,254 cycles
PAX CABIN LEFT SILL HAS MINOR CORROSION ON NUTPLATE AT FS 559.0. REMOVED NUTPLATE IAW SRM 51-42-02. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .039" ORIGINAL .050" MATERIAL REMOVED IS .011". AREA EXCEEDS LIMITS IAW SRM 53-00-00. REPLACED STRAP WITH NEW STRAP IAW SRM 51-42-06. CLASSIFIED AS MAJOR.
Part: BULKHEAD — GOUGED (BS 621) · airframe 29,669 hrs · 26,256 cycles
AFT PRESSURE BULKHEAD AT FS621.00 HAS A GAUGE ON A BRACKET ADJACENT TO CARGO DOOR TRACK. BLENDED DAMAGED BRACKET IAW SRM 51-12-00. PERFORMED NDT INSPECTION IAW REO 601R-53-61-4350 IAW NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. REPAIRED IAW REO 601R-53-61-4350.
Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 29,668 hrs · 26,254 cycles
AFT PRESSURE BULKHEAD FS 621.00 HAS THREE BROKEN ISOLATORS. R & R ISOLATORS IAW SRM 51-42-13.
Part: FLOORBEAM — CORRODED (BS 621) · airframe 29,668 hrs · 26,254 cycles
CARGO FLOORBEAM AT FS 621.00 AND BETWEEN RBL 27-45 CORRODED. BLENDED CORROSSION IAW SRM 51-21-06. ORIGINAL MATERIAL .093 MINIMUM REMAINING MATERIAL IS .089 FOUND TO BE IN LIMITS REF SRM 53-00-00. RESTORED FINISH TO AREA REF SRM 51-21-16.
Part: RIB — CRACKED (LT PYLON) · airframe 29,668 hrs · 26,254 cycles
RIB CRACKED BESIDE NUTPLATE FOR LT PYLON ACCESS PANEL 412AB. REPAIRED IAW REO 601R-54-61-073
Part: SUPPORT BRACKET — CORRODED (BS 349) · airframe 29,668 hrs · 26,254 cycles
CRAWLWAY PANEL SUPPORT BRACKET AT FS 349 CORRODED. REMOVED CRAWLWAY PANEL SUPPORT BRACKET IAW SRM 51-42-06. DRILLED NEW BRACKET IAW SRM 51-42-06. INSTALLED NEW CRAWLWAY SUPPORT BRACKET IAW SRM 51-42-06.
Part: FRAME — CORRODED (BS 333) · airframe 29,669 hrs · 26,256 cycles
GROUND WIRE STUD AT FS 333, S26R CORRODED. REMOVED AND REPLACED FRAME IAW SRM 51-42-06.
Part: ANGLE — CORRODED (BS 319.7-349) · airframe 29,669 hrs · 26,256 cycles
SERVICE DOOR SILL IS CORRODED FROM FS 319.7 - 349. BLENDED CORROSION IAW SRM 51-21-06. REMOVED IAW SRM 53-00-00. INSTALLED THRESHOLD LOWER ANGLE IAW SRM 51-40-11 & 51-42-06.
Part: PLACARD — TORN (PAX DOOR) · airframe 29,668 hrs · 26,254 cycles
PAX DOOR EXIT PLACARD IS TORN. REMOVED TORN PLACARD IAW AMM 11-30-00-000-801. INSTALLED SERVICEABLE PLACARD IAW AMM 11-30-00-400-801.
Part: FRAME — CORRODED (BS 349) · airframe 29,668 hrs · 26,254 cycles
FRAME AT FS 349 CORRODED BETWEEN S24L TO 24R. DRILLED UP NEW FRAME IAW SRM 51-40-11. REMOVED AND REPLACED FRAME IAW SRM 51-42-06.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 29,282 hrs · 25,855 cycles
UPON ARRIVAL OF ACFT FOUND EMERGENCY LIGHT SWITCH ON. OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,488 hrs · 24,996 cycles
NR 2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. RELAMPED NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21.
Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 28,283 hrs · 24,785 cycles
ALL EMERGENCY LIGHTS ARE INOP. WORK COMPLETED IAW ITEM: 1. CHARGED ALL EMERGENCY BATTERY PACKS IAW CMM 33-42-12. OPS CHECK GOOD. (CLOSED)
Part: BRACKET — BENT (MLG) · airframe 28,004 hrs · 24,471 cycles
ON T/O WHEN GEAR HANDLE SELECTED UP NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGES ILLUMINATED. COMPLIED W/ QRH RETURNED TO ATL A/C RETURNED. FOUND NLG CENERING PROS SWITCH BRACKET BENT REPALCED BRACKET IAW CMM 32-20-04 C/W EXTENSION /RETRACTON OF THE NOSE & MAIN GEAR IAW AMM 32-30-00-720-801 OPS CHECKED GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,957 hrs · 24,417 cycles
NR 3 CEILING EMERGENCY LIGHT IN CABIN INOP. RELAMPED NR 3 CEILING EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECK GOOD. (CLOSED)
2010
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,424 hrs · 23,797 cycles
RT EXTERIOR THIRD FROM FRONT EMERGENCY LIGHT INOP. R & R RT EXTERIOR EMERGENCY LIGHT 3RD FROM FRONT IAW AMM 33-51-21. OPS CK GOOD. R & R RT EXTERIOR EMERGENCY LIGHT 3RD FROM FRONT IAW AMM 33-51-21. OPS CK GOOD. (CLOSED)
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 27,133 hrs · 23,449 cycles
RETRACTED FLAPS FROM 20 DEGREE SETTING AFTER TAKEOFF BUT FLAPS FAILED AT 8 DEGEE QHR PROCEDURES COMPLIED WITH FLAPS 8 DEGREE LANDING AT 300 FPM. DESCENT RATE ON TOUCHDOWN (ENROUTE TO MEM ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED) R & R FECU IAW AMM 27-51-05, OPS CHECK GOOD ACFT OK FOR SERVICE.
Part: PIN — DAMAGED (PAX DOOR) · airframe 27,024 hrs · 23,332 cycles
MAIN PAX DOOR WILL NOT OPEN. REPLACED PIN ON HANDRAIL DOOR. OPS CHECK GOOD IAW AMM 52-10-01. (CLOSED)
Part: COALESCER BAG — CONTAMINATED (CABIN AIR) · airframe 26,928 hrs · 23,216 cycles
EXCESS FOG IN FLIGHT DECK FROM AIR VENTS. CLEANED RT PACK COALESCER IN RT WATER SEPERATOR IAW AMM 21-51-13.3 OPS CHECKED GOOD IAW AMM. OK FOR SERVICE. (CLOSED)
Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 26,874 hrs · 23,160 cycles
LIGHTS OUT: A/C AVAIL, LT BOOST PUMP INOP, LT CROSSFLOW SWITCH, LT 10TH STAGE BLEED, PACK LIGHTS, EMERGENCY LIGHTS. R & R BULBS IAW ESPM 20-24-00. (CLOSED)
Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 26,649 hrs · 22,900 cycles
EMERGENCY EXIT SIGN AT THE FWD LOWER POSITION BY THE SERVICE DOOR IS BROKEN. R & R EMERGENCY EXIT SIGN AT THE FWD LOWER POSITION BY THE SERVICE DOOR IAW AMM 33-24-08, OPS CHECK GOOD. ITEM: 1/ R & R EMERGENCY EXIT SIGN AT THE FWD LOWER POSITION BY THE SERVICE DOOR IAW AMM 33-24-08, OPS CHECK GOOD.
Part: POST — CRACKED (BS 409) · airframe 26,042 hrs · 22,197 cycles
CONTINUATION OF MWC 8731715/150, FOUND FS 409+128 VERT POST BL 0. LT SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-41-1160 IAW REO 601R-53-41-1160. APPLIED CORROSION INHIBITOR WHERE REQUIRED. INSTALLED AIR DUCT IAW 51-41-02.
Part: BULKHEAD — CRACKED (BS 621) · airframe 26,042 hrs · 22,197 cycles
AFT PRESSURE BULKHEAD WL 103.5 RBL 27.50 AND RBL 36.20 HAS NDT INDICATION NOTED APPROX .250" IN LENGTH 90 PERCENT. UPON REMOVAL OF FASTENERS IN STEP 3 OF MAINT ACTION OF MWC 315 FOUND 2EA INTERPITCHED RIVETS IN Z-MEMBER WHICH WERE GIVING NDT INDICATIONS REPAIRED IAW REO 601R-53-61-3520. REQUIRES PRIMER AND PAINT. PRIMED AND PAINTED REPAIRED AREAS IAW REO NR 601R-53-61-3520 STEP 4. INSTALLATION OF PLT214-5/PLT214-6 BLIND BOLTS INSTEAD OF MS204-70A5 RIVETS ON PRESSURE BULKHEAD COMPLETED IAW REO 601R-53-61-3521 AND MEETS WITH ALL ITS REQUIREMENTS. DISPOSITION FOR LOW PITCH CONDITION ON BULKHEAD IS COMPLETED IAW REO 601R-53-61-3520 AND MEETS WITH ALL ITS REQUIREMENTS.
Part: POST — CRACKED (BS 409) · airframe 26,042 hrs · 22,197 cycles
CONTINUATION OF CO NR 7317110 8731715 OP 151 FOUND FS 409.0+128 VERTICAL POST RBL 18 INBD AND OTBD SIDE HAVE INDCIATIONS NOTED APPROX .2" LEGNTH 60 PERCENT FSH AT WL 69 AFT FLANGE RADIUS FAILED NDT. PAINTED AREA IAW SRM 51-25-16 AND APPLIED CORROSION PREVENTATIVE TO AREA IAW SRM 51-21-11 REPAIR D1A. COMPLIED WITH EC/TC REO 601R-53-41-889.
Part: ATTACH FITTING — CRACKED (BS 460) · airframe 26,033 hrs · 22,187 cycles
MAIN CABIN FS 460.0 AT RBL 9.0 INTERCOSTAL ATTACH FITTING CRACKED IN RADIUS ON AFT SIDE. OK TO CLOSE 165BZ AND 165DZ. INSTALLED SCREWS & HARDWARE FOR FIVE WIRE BUNDLE SUPPORT MOUNTING BRACKETS. REINSTALLED FLOOR PANEL ACCESS PANELS (165BZ/165DZ) IAW SRM 51-41-02. REINSTALLED ADEL CLAMPS REMOVED ON ITEM 4. REINSTALLED IAW SRM 51-41-02. APPLIED CORROSION PREVENTATIVE TO REPAIR IAW SRM 51-21-11.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,033 hrs · 22,187 cycles
AFT PRESSURE BULKHEAD WL103.5 RBL27.50 AND RBL36.20 HAS NDT INDICATIONS NOTED APPROX .250" IN LENGTH 90 PERCENT FSH. REMOVED 3 EA LINER SUPPORTS FROM F.S. 621 BULKHEAD AT RBL 36 IAW SRM 51-42-06 PAR. 11. REINSTALL 3 EA SUPPORTS. REINSTALLED 3 EA LINER SUPPORTS IAW SRM 51-42-06 1A, 7B1, 9A1 & C1. REMOVED RIVETS IN FS 621 PRESSURE BULKHEAD WEB AT RBL 36. REPAIR AREA AND REMOVED FWD ANGLE ON FS 621 BULKHEAD WEB FROM LBL 36 TO RBL 46 TO FACILITATE BULKHEAD REPAIR IAW SRM 51-42-06. INSTALL REMOVED FASTENERS AND ANGLE. REINSTALLED FASTENERS IN RBL 27 & RBL 36 Z MEMBERS. REINSTALLED FASTENER IN FWD FS 621 ANGLE FROM LBL 27 TO RBL 36 IAW SRM 51-42-06 1A, 7B1, C1 & 9A1, C1. REMAINING FASTENER AT RBL 36 OTBD REQUIRE INSTALL. INSTALLED REMAINING FASTENERS IAW REO 601R-53-61-3521 CONTINUED ON CO NR 7317110 JOB NR 8731711 OP NR 327. CLOSED
Part: FINGER DOUBLER — CORRODED (BS 409-559) · airframe 26,033 hrs · 22,187 cycles
CONTINUATION OF CO NR 7317110 JOB NR 8731711, OP NR 251, MAIN CABIN BETWEEN FS 409+128 & FS 559.00 PRESSURE FLOOR SILL FINGER WEB DOUBLER HAS NUMEROUS AREAS OF CORROSION ON LT SIDE. COMPLIED WITH REO 601R-53-41-666 REV O.
Part: POST — CRACKED (BS 409) · airframe 26,033 hrs · 22,187 cycles
FOUND FS 409.0+128 VERTICAL POST RBL 18.0 INBD AND OTBD SIDES HAVE INDICAITONS NOTED APPROX .2" IN LENGTH 60 PERCENT FSH AT WL 69 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED INBD & OTBD POST IAW SRM 51-42-06, STEP 11. DRILLED & INSTALLED. LOCATED, DRILLED AND ASSEMBLED POST HALVES IAW SRM 51-40-11 AND 51-42-06 PAR B & PAR 9A(1). INSTALLED POST ASSY IAW SRM 51-42-06 & ECTC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889. SEALED VERTICAL POST IAW SRM 51-23-00, PG 6, ITEMS 5A(1) THROUGH (3), PG 7 ITEMS 6A THROUGH B(1), PG 10 ITEMS 7B(1) THROUGH (6).
Part: SKIN — CRACKED (RT WING) · airframe 26,033 hrs · 22,187 cycles
FOUND RT LOWER WING PLANK FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED INBD SIDE OF LANDING IN NON CRITICAL AREA APPROX .5" IN LENGTH 90 PERCENT AND 50 PERCENT FSH FAILED NDT INSPECTION. MARKED ON ACFT. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV G AND FWD ALL REQUIREMENTS TO ASA STRUCTURES ENGINEERING.
Part: BULKHEAD — CRACKED (BS 621) · airframe 26,033 hrs · 22,187 cycles
FS 621.00 PRESSURE BULKHEAD FWD FACE HAS AN 80 PERCENT FSH HFEC INDICATION NOTED APPROX 0.50" LONG EXTENDING FROM THE UPPER CORNER OF THE AFT CARGO DOOR TRACK AT LBL 27.50 APPROX WL 131.00. COMPLIED WITH EC/TC REO 601R-53-61-1541.
Part: POST — CRACKED (BS 409) · airframe 26,033 hrs · 22,187 cycles
FOUND FS 409+128 VERT POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 % FSH AFT FLANGE RADIUS. FAILED NDT INSP. DISCONNECTED AIR DUCTS IAW SRM 51-41-02 FOR ACCESS TO POST. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED AND ASSEMBLED POST IAW SRM 51-40-11 AND 51-42-06. INSTALLED POST ASSY LT REINFORCEMENT ANGLE AND AIR DUCTS. INSTALLED POST ASSY IAW SRM 51-42-06 AND REO 601R-53-41-1160. FILLET SEAL POST ASSY TOUCH-UP PAINT AREA. LOCATED AND INSTALL LT REINFORCEMENT ANGLE AND INSTALL AIR DUCTS. INSTALLED REINFORCEMENT ANGLE IAW SRM 51-42-06 AND REO 601R-53-41-1160. FILLET SEALED POST IAW SRM 51-23-00 & RESTORED PAINT FINISH IAW STILL REQUIRES AIR DUCT INSTALL.
Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 26,033 hrs · 22,187 cycles
LT FLOOR SEAT TRACKS FROM FS 409 TO FS 559.0+80 ARE CORRODED. REMOVED CORRODED SEAT TRACK LT FS 409 TO FS 559.0+80 IAW AMM 53-01-11-000-802 STEP 3, B(1)(2)(3). INSTALLED NEW SERVICEABLE SEAT RAIL FS 409 TO FS 559.0+80 LT IAW AMM 53-01-11-400-802, STEP 2B (1)(2)(3)(4)(5)(6)(7) AND (8).
Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 26,033 hrs · 22,187 cycles
RT FLOOR SEAT TRACKS FROM FS 409 TO FS 559 ARE CORRODED. REMOVED CORRODED SEAT TRACK FROM FS 409 TO FS 559 RBL 9.0 IAW AMM 53-01-11000-802, PG 401, STEP 3.B.(1)(2)(3). INSTALLED NEW TRACK FROM FS 409 TO FS 559 RBL 9.0 IAW AMM 53-01-11-400-802 PG 406 STEP 2.B.(1) THRU (8).
Part: FLOORBEAM — CORRODED (BS 559) · airframe 26,033 hrs · 22,187 cycles
FLOOR SUPPORT TRANSVERSE BEAM FROM RBL 9 TO RBL 18 AT FS 559.0+80 HAS CORROSION. R & R FLOOR SUPPORT TRANSVERSE BEAM FROM RBL9 TO RBL18 AT FS 559.0+80, IAW SRM 51-42-06, STEP 11, 51-46-06 STEP 9 A & B & 51-42-10.
Part: FLOORBEAM — CORRODED (BS 605) · airframe 26,033 hrs · 22,187 cycles
RT FLOOR EDGE MEMBER IS CORRODED AT FS 605 RBL 36. REMOVED APPROX .002 CORROSION FROM RT FLOOR EDGE MEMBER IAW SRM 51-21-06. BLENDED AREA WITHIN LIMITS IAW SRM 53-00-00, PG 106, FIG 102 SHEET 2. BLENDED AREA. TREATED, PRIMED, AND PAINTED AREA IAW SRM 51-21-11, 51-25-06, AND 651-25-16.
Part: WEB — CORRODED (BS 409-559) · airframe 26,033 hrs · 22,187 cycles
MAIN CABIN RT SIDE BETWEEN FS 409+128 & FS 559.00 PRESSURE FLOOR SILL WEB HAS NUMEROUS AREAS OF CORROSION. REMOVED CORROSION FROM PRESSURE FLOOR SILL WEB IAW REO 601R-53-41-666 AND SRM 51-21-06. COMPLIED WITH REO 601R-53-41-666A. PERFORMED EDDY CURRENT OF REPAIRED AREA OF RT SIDE PRESSURE FLOOR SILL IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. RESTORED FINISH OF REPAIRED AREAS IAW ITEM 6 OF REO 601R-53-41-666. RESTORED SEALANT ALONG SILL IAW STEP 7 OF REO 601R-53-41-666. APPLIED CORROSION INHIBITING COMPOUND IAW ITEM 8 OF REO 601R-53-41-666. COMPLIED WITH REO 601R-53-41-666 REV O DATED 27 MAY, 2008.
Part: FINGER DOUBLER — CORRODED (BS 409-559) · airframe 26,033 hrs · 22,187 cycles
MAIN CABIN BETWEEN FS 409+128 & FS 559.00 PRESSURE FLOOR SILL FINGER WEB DOUBLER HAS NUMEROUS AREAS OF CORROSION ON LT SIDE. REMOVED CORROSION FROM PRESSURE FLOOR SILL FINGER DOUBLER IAW REO 601R-53-41-666 AND SRM 51-21-06. COMPLIED WITH REO 601R-53-41-666A. PERFORMED EDDY CURRENT OF REPAIRED AREAS LT SIDE PRESSURE FLOOR SILL DOUBLER IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. RESTORED FINISH OF REPAIRED AREA IAW ITEM 13 OF REO 601R-53-41-666. RESTORED SEALANT BEAD TO REPAIRED AREA IAW ITEM 14 OF REO 601R-53-41-666. APPLIED CORROSION INHIBITING COMPOUND TO REPAIRED AREA IAW ITEM 15 OF REO 601R-53-41-666.
Part: ATTACH FITTING — CRACKED (BS 460) · airframe 26,033 hrs · 22,187 cycles
MAIN CABIN FS 460.00 AT RBL 9.00 INTERCOSTAL ATTACH FITTING CRACKED IN RADIUS ON AFT SIDE. REMOVED INTERCOSTAL FROM ACFT. INSTALLED INTERCOSTAL IAW SRM 51-42-21 AND SRM 51-42-06.
Part: SILL — CORRODED (BS 409-559) · airframe 26,033 hrs · 22,187 cycles
MAIN CABIN LT SIDE BETWEEN FS 409+128 & FS 559.00 PRESSURE FLOOR SILL WEB HAS NUMEROUS AREAS OF CORROSION. REMOVED CORROSION FROM PRESSURE FLOOR SILL WEB IAW REO 601R-53-41-666 & SRM 51-21-06. COMPLIED WITH REO 601R-53-41-666A. PERFORMED EDDY CURRENT OF REPAIRED AREAS IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. RESTORED FINISH TO REPAIRED AREA IAW ITEM 6 OF REO 601R-53-41-666. RESTORED SEALANT BEAD ALONG SEAL EDGE IAW ITEM 7 OF REO 601R-53-41-666. APPLIED CORROSION INHIBITING COMPOUND TO REPAIRED AREA IAW ITEM 8 OF REO 601R-41-666. COMPLIED WITH REO 601R-53-41-666 REV O DATED 27 MAY, 2008.
Part: FINGER DOUBLER — CORRODED (BS 409-559) · airframe 26,033 hrs · 22,187 cycles
MAIN CABIN RT SIDE BETWEEN FS 409+128 & FS 559.00 PRESSURE FLOOR SILL FINGER WEB DOUBLER HAS NUMEROUS AREAS OF CORROSION. REMOVED CORROSION FROM PRESSURE FLOOR SILL FINGER DOUBLER IAW REO 601R-53-41-666 AND SRM 51-21-06. COMPLIED WITH REO 601R-53-41-666A. PERFORMED EDDY CURRENT OF REPAIRED AREAS OF RT SIDE PRESSURE FLOOR SILL DOUBLER IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. RESTORED THE REPAIRED AREA IAW ITEM 13 OF REO 601R-53-41-666. RESTORED THE SEALANT ALONG SILL EDGE IAW TIEM 14 OF REO 601R-53-41-666. APPLIED CORROSION INHIBITING COMPOUND TO REPAIRED AREAS IAW ITEM 15 OF REO 601R-53-41-666. COMPLIED WITH REO 601R-53-41-666 REV O DATED 27 MAY, 2008
Part: STRUCTURE — CORRODED (BS 605) · airframe 26,033 hrs · 22,187 cycles
CARGO COMPARTMENT BELOW FLOOR FS 605.00 BETWEEN S26 & 27L FRAME FWD SIDE ATTACH FLANGE AROUND FASTENERS HAS CORROSION. REPAIRED FRAME AT FS 605.00 BETWEEN S26L AND S27 IAW SRM 53-00-15 REPAIR 2.
Part: FLOORBEAM — CORRODED (BS 574-621) · airframe 26,033 hrs · 22,187 cycles
CARGO COMPARTMENT BETEEN FS 574.00 & FS 621.00 LBL 27.00 FLOORBEAM UPPER CAP HAS CORROSION GROUND FASTENER HOLES. REMOVED 7 EA BOLTS AND 2 EA PINS FROM PULLEY BRACKET AT FS 621, LBL 27 AND REMOVED PULLEY BRACKET FOR ACCESS. CABLE TENSION NOT AFFECTED. REMOVED FLOORBEAM CAP FROM FS 574-FS 621 IAW SRM 51-42-06 AND 51-42-21. NEW FLOORBEAM CAP REQUIRES INSTALL AND PULLEY BRACKET REQUIRES RE-INSTALL. INSTALLED FLOORBEAM CAP AND PULLEY BRACKET ASSY IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-45-00, 51-42-34, 51-41-02 & REO 601R-53-61-3494. COMPLIED WITH EC/TC REO 601R-53-61-3494 AND REO 601R-53-61-3494 REV.
Part: SUPPORT ANGLE — CRACKED (BS 469.63-476.67) · airframe 26,032 hrs · 22,187 cycles
LT SIDE ACCESS PANEL 161EL SUPPORT ANGLES CRACKED AT FS 469.63 AND 476.67. R & R 161EL SUPPORT ANGLES AT FS 469.63 AND 476.67 IAW SRM 51-40-11, 51-42-06, AND 51-42-21. (CLOSED)
Part: PLACARD — WORN (ESCAPE HATCH) · airframe 26,033 hrs · 22,187 cycles
CREW ESCAPE HATCH PLACARDS ARE WORN. (OPEN)
Part: SUPPORT ANGLE — CRACKED (BS 469.63-476.67) · airframe 26,033 hrs · 22,187 cycles
LT SIDE ACCESS PANEL 161EL SUPPORT ANGLES CRACKED AT FS 469.63 AND 476.67. (OPEN)
Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 26,032 hrs · 22,187 cycles
ADJUSTED RT EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-001 SECTION A2 TO A6 AND AMM 51-21-00-863-004. DISPOSITION OF THE LOW GAP CLEARANCE BETWEEN AFT TOP CORNER AND RT SIDE EMER EXIT DOOR ON A/C S/N 7317 IS COMPLETED IAW REO 601R-52-21-051 AND MEETS WITH ALL ITS REQUIREMENTS. ASA RII C/W: 5300007.
Part: PLACARD — WORN (ESCAPE HATCH) · airframe 26,032 hrs · 22,187 cycles
APPLIED NEW SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801.
Part: HANDLE — OUT OF TOLERANCE (EMERGENCY EXIT) · airframe 26,033 hrs · 22,187 cycles
RT EMERGENCY EXIT FAILS FUNCTION TEST, HANDLE RELEASES AT 50-55 LBS. ADJUSTED RT EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-001 SECTION A2 TO A6 AND AMM 51-21-00-863-004. DISPOSITION OF THE LOW GAP CLEARANCE BETWEEN AFT TOP CORNER AND RT SIDE EMERGENCY EXIT DOOR COMPLETED IAW REO 601R-52-21-051 AND MEETS WITH ALL ITS REQUIREMENTS.
Part: ANGLE — CRACKED (BS 625) · airframe 26,033 hrs · 22,187 cycles
RT AND LT FS 625 OBLIQUES ARE CRACKED. OPEN
Part: ANGLE — CRACKED (BS 625) · airframe 26,032 hrs · 22,187 cycles
RT AND LT FS 625 OBLIQUES ARE CRACKED. REMOVED FS 625.00 RT AND LT OBLIQUE ANGLES IAW SRM 51-42-21 SECTION 11(A-B). OBTAINED SERVICEABLE ANGLES AND PREPARED FASTENER HOLES IAW SRM 51-42-21 SECTION 5(A) AND INSTALLED IAW SRM 51-42-21 SECTION 9(A-C). (CLOSED)
2009
Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 26,011 hrs · 22,160 cycles
R & R NR1 AND NR2 CHARGER ASSY IAW AMM 33-51-05. OPS CHECK IAW AMM 33-51-04. (CLOSED)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,012 hrs · 22,160 cycles
AFTER LEAVING GATE F/A ADVISED EXIT ROW EMERGENCY WOULD NOT ILLUMINATE DURING PRE T/O BRIEFING.
Part: FLASHLIGHT — BROKEN (CABIN) · airframe 25,944 hrs · 22,085 cycles
F/O 'S FLASHLIGHT BROKEN.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,879 hrs · 20,005 cycles
CABIN FORWARD MOST CEILING EMERGENCY LIGHT INOP, CABIN EMERGENCY LIGHTS - CEILING LEVEL EMERGENCY FLOOD LIGHTS. REMOVED AND REPLACED CHARGER. CHECK GOOD.
Part: MOTOR — INOPERATIVE (PAX DOOR ASSIST) · airframe 22,863 hrs · 19,128 cycles
AIRSTAIR DOOR WILL NOT OPEN REMOVED AND REPLACED CABIN DOOR ASSIST MOTOR IAW AMM 52-11-00, DEFER CLEARED, PLACARD REMOVED. (B)
Part: MOTOR — INOPERATIVE (DOOR ASSIST) · airframe 2,282,950 hrs · 19,098 cycles
ASD WILL NOT OPEN. (PASSENGER DOOR POWER ASSIST SYSTEM). REMOVED AND REPLACED CABIN DOOR ASSIST MOTOR IAW AMM 52-11-00. DEFER CLEARED, PLACARD REMOVED. (S)
Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 22,736 hrs · 19,024 cycles
FLAP FAIL AT 8 DEGREES (EN ROUTE TO ATL ACFT DIVERTED TO MDT DUE TO MTC, EMERGENCY DECLARED). PERFORMED EXTERNAL VISUAL CHECK OF FLAPS IN ALL SETTINGS. NO TWISTING OR SKEWING DETECTED. CYCLED FLAPS MULTIPLE TIMES WITH NO FURTHER FAULTS NOTED. INTERROGATED FECU AND NO CURRENT FAULTS EXIST IAW TEMP REV 27-01 AND FIM 27-50-00, AC OK FOR SERVICE. (S)
Part: PDU — OUT OF RIG (TE FLAPS) · airframe 2,269,151 hrs · 18,980 cycles
FLAPS FAILED IN FLIGHT AT 20. BOTH FLAPS INDICATED 20 ON THE SYNOPTIC PAGE, BOTH FLAPS OUTLINED IN YELLOW ON SYNOPTIC PAGE. FLAPS WERE LOWERED AT AIRSPEED OF 180KNOTS. COMPLIED WITH QRH, NO UNUSUAL CONTROL FEEL---[EMERGENCY DECLARED] REMOVED & REPLACED PDU AND RIGGED LT BPSU. OPS CHECK GOOD REMOVED AND REPLACED PDU IAW AMM 27-52-01, OPS CHECK GOOD
Part: BPSU — INOPERATIVE (TE FLAPS) · airframe 2,269,725 hrs · 18,985 cycles
FLAPS FAILED AT 20 DEGREES DURING APPROACH INTO FSM. REMOVED AND REPLACED RT BPSU IAW AMM 27-51-10 COMPLIED WITH PER SP 607 AND AMM 27-51-10 WORK SATISFACTORY. PERFORMED RIGGING OF SYSTEM. OPS CHECK GOOD ON FLAP SYSTEM AT THIS TIME. (B)
Part: FITTING — CRACKED (FUSELAGE) · airframe 22,083 hrs · 18,426 cycles
AAR - O/B CLIP AT FS 280 RBL 9 CRACKED. REMOVED CRACKED RBL 9 O/B FS 280 CLIP. REF FORM 412 FOR FABRICATION OF SERVICEABLE CLIP FOR RBL 9 O/B AT FS 280. REF REO 601R-53-11-171 FOR MATERIAL TYPE. INSTALLED SERVICEABLE CLIP IAW CRJ200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/08.
Part: FITTING — CRACKED (FUSELAGE) · airframe 22,083 hrs · 18,426 cycles
AAR - 1016 - I/B CLIP AT FS 280 RBL 9 CRACKED. REMOVED CRACKED RBL 9 I/B CLIP AT FS 280. REF FORM 412 FOR FABRICATION OF SERVICEABLE CLIP FOR RBL 9 I/B AT FS 280. REF REO 601R-53-11-171 FOR MATERIAL TYPE. INSTALLED SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/08.
Part: FITTING — CRACKED (FUSELAGE) · airframe 22,083 hrs · 18,426 cycles
AAR - RIGHT 484 O/B RBL 27 CLIP CRACKED. REMOVED CRACKED CLIP FROM RT 484 O/B RBL 27. REF FORM 412 FOR FABRICATION OF SERVICEABLE CLIP IAW CRJ SRM 53-41-43. INSTALLED SERVICEABLE CLIP IAW CRJ SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/08.
Part: FITTING — CRACKED (FUSELAGE) · airframe 22,083 hrs · 18,426 cycles
AAR - 1017 - I/B CLIP AT FS 280 LBL 9 CRACKED. REMOVED CRACKED LBL 9 I/B CLIP AT FS 280. REF FORM 412 FOR FABRICATION OF SERVICEABLE CLIP FOR LBL 9 I/B CLIP AT FS 280 REF REO 601R-53-11-171 FOR MATERIAL TYPE. INSTALLED SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/08.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,083 hrs · 18,426 cycles
FWD FLOOR SUPPORT ANGLE AT FS 280 CRACKED LEFT SIDE. REMOVED FWD FLOOR SUPPORT ANGLE. LOCATED HOLES ON SERVICEABLE FWD ANGLE PN 600-34017-351 IAW SRM 51-40-11. OK TO INSTALL INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06. OK APPLY FINISH A023 TO FASTNERS. APPLIED FINISH TO FASTNERS IAW 200 SRM 51-21-16
2007
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,916 hrs · 18,285 cycles
NR 3 EPSU BATTERY PACK IS DEAD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,916 hrs · 18,285 cycles
NR 4 EPSU BATTERY PACK IS DEAD.
Part: DOOR — INOPERATIVE (SERVICE) · airframe 20,713 hrs · 17,296 cycles
SERVICE DOOR DOES NOT CLOSE.
Part: HYDRAULIC SYSTEM — LOW PRESSURE (NR 2 SYSTEM) · airframe 20,702 hrs · 17,284 cycles
JAN - DCA DIVERTED INTO ROA HYD SYSTEM NR 2 HIGH TEMP CAUTION MSG AND THEN LOST PRESSURE. CAPT SHUT THE ENGINE DOWN, QTY AT 15 PERCENT AFTER LANDING. EN ROUTE TO DCA A/C DIVERTED TO ROA DUE TO MTC. EMERGENCY DECLARED. FLT 4459 CX AND ON 5/12/07 FLT 4623 CX.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,027 hrs · 16,788 cycles
AFT PRESSURE BULKHEAD IS CRACKED ADJACENT TO THE CARGO COMPARTMENT DOOR LINTEL ATTACHMENT FITTING. COMPLIED WITH N/R-00001 AFT PRESSURE BULKHEAD REPAIR AT LINTED ATTACH FITTING, IAW REO 601R-53-61-1230. COMPLIED WITH EC/TC REO 601R-53-61-1230.
2006
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,715 hrs · 16,566 cycles
FLOOR EMERG LIGHTING STRIP AT 8C INOP.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,315 hrs · 15,431 cycles
WITH EMERGENCY LIGHTS IN ARM POSITION, EMERGENCY LIGHT CAME ON.
Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 17,995 hrs · 15,178 cycles
NLG STEERING MSG CAME ON AFTER TAKEOFF, FLT 4251 CX AN EMERGENCY WAS DECLARED.
Part: STRUCTURE — CORRODED (FUSELAGE)
DURING C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 530, RBL 42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 530, RBL 42, IAW REO. (K)
Part: UNKNOWN — CORRODED (BS 459)
DURING A C-CHECK IN MCN, CORROSION FOUND AROUND THE NUT PLATE AT FS 459, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 459, LBL 42, IAW REO. (K)
Part: ECU — MALFUNCTIONED (NLG STEERING)
DURING CRUISE, UPON GEAR RETRACTION, THE CREW RECEIVED AN AMBER CAUTION MESSAGE (STEERING INOPERATIVE) MESSAGE ON THE ED1. THE CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY AND THE AIRCRAFT DIVERTED, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING ECU, AND ALSO RERIGGED THE RT FEEDBACK RVDT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: FLOOR SUPPORT — CORRODED (BS 313-346)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE SERVICE DOOR SILL FLOOR SUPPORT ANGLE, AT FS 313-346. (M) AFTER MAINTENANCE BLERIDED, ALODINED, AND PRIMED THE SERVICE DOOR SILL FLOOR SUPPORT ANGLE, AT FS 313-346, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. (K)
Part: FLOOR SUPPORT — CORRODED (BS 350)
DURING A C-CHECK IN MCN, CORROSION WAS FOUND ON THE FLOOR SUPPORT WEB, AT FS 350, RBL 44. (M) AFTER MAINTENANCE BLENDED, ALODINED, AND PRIMED THE FLOOR SUPPORT WEB, AT FS 350, RBL 44, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. (K)
Part: UNKNOWN — UNKNOWN (BS 718)
DURING C-CHECK, A SUSPECTED CRACK WAS FOUND ON THE LT SIDE OF FS 718. MAINTENANCE REPAIRED THE CRACK ON THE LT SIDE OF FS 718 IAW REO. (K)
Part: SILL — CORRODED (FUSELAGE)
DURING A C-CHECK IN MCN, CORROSION WAS FOUND ON THE LOWER SERVICE DOOR SILL CORNER ANGLE, AT FS 348. (M) MAINTENANCE REPAIRED THE LOWER SERVICE DOOR SILL CORNER ANGLE, AT FS 348, IAW SRM. (K)
Part: ANGLE — CORRODED (FS 311)
DURING C-CHECK, CORROSION WAS FOUND ON THE SERVICE DOOR LOWER SILL FORWARD CORNER ANGLE, AT FS 311. MAINTENANCE DETERMINED AFTER FURTHER INSPECTION THAT THE SERVICE DOOR LOWER SILL FORWARD CORNER ANGLE, AT FS311, WAS NOT CORRODED. (K)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FLOOR BEAM END, AT FS 34B, RBL 44. MAINTENANCE REPAIRED THE TRANSVERSE FLOOR BEAM END, AT FS 346, RBL44, IAW REO. (K)
Part: NUT PLATE — CORRODED (FS536,LBL42)
DURING A C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 536, LBL42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 536, LBL 42, IAW REO. (K)
Part: SEAT TRACK — CORRODED (BS 361-409)
DURING A C-CHECK IN MCN, THE LEFT SIDEWALL SEAT TRACK, AT FS 361-409 PLUS 16, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDEWALL SEAT TRACK, AT FS 361-409 PLUS 16, IAW CRJ AMM 53-00-47. (M)
Part: UNKNOWN — CORRODED (BS 557)
DURING A C-CHECK IN MCN, FOUND CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 557, RBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 557, RBL 42, IAW REO. (K)
Part: STRUCTURE — CORRODED (FUSELAGE)
DURING C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 531, LBL 42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 531, LBL 42, IAW REO. (K)
Part: UNKNOWN — CORRODED (BS 427)
DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE NUT PLATE AT FS 427, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 427, LBL 42, IAW REO. (K)
Part: SEAT TRACK — CORRODED (BS 546-559)
DURING A C-CHECK IN MCN, THE LEFT SIDEWALL SEAT TRACK, AT FS 546-559 PLUS 80, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDEWALL SEAT TRACK, AT FS 546-559 PLUS 80, IAW CRJ AMM 53-00-47. (M)
Part: STRUCTURE — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 550, RBL42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 550, RBL42, IAW REO. (K)
Part: SEAT TRACK — CORRODED (BS 409)
DURING A C-CHECK IN MCN, THE LEFT SIDEWALL SEAT TRACK, AT FS 409 PLUS 16 - 409 PLUS 112, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDEWALL SEAT TRACK, AT FS 409 PLUS 16 - 409 PLUS 112, IAW CRJ AMM 53-00-47. (M)
Part: STRUCTURE — CORRODED (BS 478)
DURING A C-CHECK IN MCN, CORROSION FOUND AROUND THE NUT PLATE AT FS 478, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 478, LBL 42, IAW REO. (K)
Part: STRUCTURE — CORRODED (BS 486)
DURING A C-CHECK IN MCN, THE CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 486, LBL 42. (M)
Part: UNKNOWN — CORRODED (BS 536)
DURING A C-CHECK IN MCN, FOUND CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 536, RBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 536, RBL42, IAW REO. (K)
Part: UNKNOWN — CORRODED (BS 447)
DURING A C-CHECK IN MCN, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 447, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 447, LBL 42, IAW REO. (K)
Part: UNKNOWN — CORRODED (BS 435)
DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE NUT PLATE AT FS 435, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 435, LBL 42, IAW REO. (K)
Part: SEAT TRACK — CORRODED (BS 500-547)
DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SIDEWALL SEAT TRACKS, AT FS 500-547, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SIDEWALL SEAT TRACKS, AT FS 500-547, IAW CRJ AMM 53-00-47. (M)
Part: SEAT TRACK — CORRODED (BS 409)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE RIGHT SIDEWALL SEAT TRACK AT FS 409 PLUS 16-409 PLUS 112. (M) MAINTENANCE REMOVED AND REPLACED THE RT SIDEWALL SEAT TRACK AT FS409+16-409+112, IAW SRM. (K)
Part: STRUCTURE — CORRODED (FUSELAGE)
DURING C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 450, RBL 42. MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 450, RBL 42, IAW REO. (K)
Part: STRUCTURE — CORRODED (BS 468)
DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE NUT PLATE AT FS 468, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 468, LBL 42, IAW REO. (K)
Part: UNKNOWN — CORRODED (BS 530)
DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE NUT PLATE AT FS 530, RBL 42. (M)
Part: FLOOR PANEL — CRACKED (BS 250-260)
DURING A C-CHECK IN MCN, THE FLIGHT COMPARTMENT FLOOR WAS FOUND TO BE CRACKED BETWEEN FS 250-260, SEVEN INCHES OUTBOARD OF FIRST OFFICERS SEAT TRACK. (M) MAINTENANCE REPAIRED THE FLIGHT COMPARTMENT FLOOR, AT FS 250-FS 260, 7 INCHES OB OF THE F/O SEAT TRACK, IAW REO. (K)
Part: SEAT TRACK — CORRODED (BS 361-394)
DURING A C-CHECK IN MCN, THE SEAT TRACK, AT FS 361-394, LBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AT FS 361-394, LBL 9, IAW CRJ SRM 51-41-00. (M)
Part: SEAT TRACK — CORRODED (BS 449-499)
DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SIDEWALL SEAT TRACKS, AT FS 449-499, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SIDEWALL SEATS TRACKS, AT FS 449-499, IAW CRJ AMM 53-00-47. (M)
Part: STRUCTURE — CORRODED (BS 542)
DURING A C-CHECK IN MCN, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 542, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 542, LBL 42, IAW REO. (K)
Part: UNKNOWN — CORRODED (BS 451)
DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE NUT PLATE AT FS 451, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 451, LBL 42, IAW REO. (K)
Part: STRUCTURE — CORRODED (BS 531)
DURING A C-CHECK IN MCN, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 531, LBL 42. (M)
Part: SEAT TRACK — CORRODED (BS 409)
DURING A C-CHECK IN MCN, FOUND CORROSION ON RIGHT SIDEWALL SEAT TRACK AT FS 409 PLUS 112-424. (M) MAINTENANCE REMOVED AND REPLACED THE RT SIDEWALL SEAT TRACK IAW SRM. (K)
Part: SEAT TRACK — CORRODED (BS 361-394)
DURING A C-CHECK IN MCN, THE SEAT TRACK, AT FS 361-394, RBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AT FS 361-394, RBL 9, IAW CRJ AMM 53-01-11. (M)
Part: SEAT TRACK — CORRODED (BS 394-409)
DURING A C-CHECK IN MCN, THE SEAT TRACK, AT FS 394-409 PLUS 128, RBL 9, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AT FS 394-409 PLUS 128, RBL 9, IAW CRJ AMM 53-01-11. (M)
Part: UNKNOWN — CORRODED (BS 441)
DURING A C-CHECK IN MCN, CORROSION FOUND AROUND THE NUT PLATE AT FS 441, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 441, LBL 42, IAW REO. (K)
Part: UNKNOWN — CORRODED (BS 541)
DURING A C-CHECK IN MCN, FOUND CORROSION AROUND THE NUT PLATE AT FS 541, RBL 42. (M) MAINTENANCE REPAIRED AORUND THE NUT PLATE AT 541, RBL42 IAW REO. (K)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLERS AT FS 513-517, LBL AND RBL 37-44. MAINTENANCE REPAIRED THE DOUBLERS AT FS 513-517, LBL AND RBL 37-44, IAW EO AND REO. (K)
Part: FINGER DOUBLER — CORRODED (FS439,BL42R)
DURING A C-CHECK, THE FINGER DOUBLER, AT FS 439, BL 42R, WAS FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: FINGER DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ONTHE FINGER DOUBLERS AT FS 538-540, LBL 44-42. MAINTENANCE REPAIRED THE FINGER DOUBLERS AT FS 538-540, LBL 44-42, IAW REO. (K)
Part: FRAME — CORRODED (BS 559)
DURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS559, RBL 38-40. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: DOUBLER — CORRODED (BS 498-513)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE DOUBLER AT FS 498-513, RBL 44-37. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 473-477, LBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 473-477, LBL 44-37, IAW REO. (K)
Part: FINGER DOUBLER — CORRODED (BS 544)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLER AT FS 544, RBL 44-41. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 427-425, LBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 427-425, LBL 44-37, IAW REO. (K)
Part: DOUBLER — CORRODED (BS 473-477)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE DOUBLER AT FS 473-477, LBL 44-37. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS498-513, RBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 498-513, RBL 44-37, IAW REO. (K)
Part: FLOORBEAM — CORRODED (BS 559)
DURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FLOORBEAM CAP AT FS559.112, RBL27-45. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: DOUBLER — CORRODED (BS 556-558)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE DOUBLER AT FS 556-558, RBL 44-42. (M)
Part: DOUBLER — CORRODED (FS 513-517)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLERS AT FS 513-517, LBL AND RBL 37-44. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: FINGER DOUBLER — CORRODED (FUSELANGE)
DURING A C-CHECK, THE FINGER DOUBLER, AT FS 439, BL 42R, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FINGER DOUBLER, AT FS 439, BL 42R IAW REO. (K)
Part: FRAME — CORRODED (BS 559)
DURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS559, LBL38-42. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: DOUBLER — CORRODED (FS 427-425)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 427-425, LBL 44-37. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 470-477, RBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 470-477, RBL 44-37, IAW REO. (K)
Part: DOUBLER — CORRODED (BS 470-477)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE DOUBLER AT FS 470-477, RBL 44-37. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 425, RBL39. MAINTENANCE REPAIRED THE DOUBLER AT FS 425, RBL 39, IAW REO. (K)
Part: DOUBLER — CORRODED (FS 467-473)
DURING C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 467-473, LBL 43-37. THE MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 467-473, LBL 43-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 467-473, LBL 43-37, IAW REO. (K)
Part: FINGER DOUBLER — CORRODED (BS 438-440)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLER AT FS 438-440, LBL 44-42. (M)
Part: FINGER DOUBLER — CORRODED (BS 447-451)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLERS AT FS 447-451, LBL AND RBL 44-42.
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE ON THE DOUBLER AT FS 543-545, LBL 44-42. MAINTENANCE REPAIRED THE DOUBLER AT FS 543-545, LBL 44-42, IAW REO. (K)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 513-517, LBL 44-37. MAINTENANCE REPAIRED THE DOUBLER AT FS 513-517, LBL 44-37, IAW REO. (K)
Part: FINGER DOUBLER — CORRODED (BS 523-530)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLERS AT FS 523-530, LBL AND RBL 44-42. (M)
Part: DOUBLER — CORRODED (BS 460-462)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 460-462, RBL 44-42. THIS WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: DOUBLER — CORRODED (BS 543-545)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE ON THE DOUBLERS AT FS 543-545, LBL 44-42. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS 460-462, RBL 44-42. MAINTENANCE REPAIRED THE DOUBLER AT FS 460-462, RBL 44-42, IAW REO. (K)
Part: FINGER DOUBLER — CORRODED (BS 538-540)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLERS AT FS 538-540, LBL 44-42. (M)
Part: FINGER DOUBLER — CORRODED (BS 540)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLER AT FS 540, RBL 44-41. (M)
Part: CAP — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS 559, LBL 38-42. (K)
Part: NUT PLATE — CORRODED (FUSELAGE)
DURING C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 542, RBL 42. MAINTENANCE REPAIRED THE NUT PLATE AT FS 542, RBL 42, IAW REO. (K)
Part: FINGER DOUBLER — CORRODED (BS 460-462)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLER AT FS 460-462, LBL 44-42. (M)
Part: FINGER DOUBLER — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ONTHE FINGER DOUBLER AT FS 544, RBL 44-41. MAINTENANCE REPAIRED THE FINGER DOUBLER AT FS 544, RBL 44-41, IAW REO. (K)
Part: CAP — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FRAME CAP AT FS 559, RBL 39-40. MAINTENANCE REPAIRED THE TRANSVERSE FRAME CAP AT FS 559, RBL 38-40, IAW REO. (K)
Part: NUT PLATE — CORRODED (FS542, RBL42)
DURING A C-CHECK, CORROSION WAS FOUND AROUND THE NUT PLATE AT FS 542, RBL 42. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K)
Part: FINGER DOUBLER — CORRODED (BS 483-485)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE FINGER DOUBLERS AT FS 483-485, LBL AND RBL 44-42. (M)
Part: CAP — CORRODED (FUSELAGE)
DURING A C-CHECK, CORROSION WAS FOUND ON THE TRANSVERSE FLOORBEAM CAP AT FS 559.112, RBL 27-45. AFTER MAINTENANCE ALODINED, PRIMED, AND BLENDED THE TRANSVERSE FLOORBEAM CAP AT FS 559, RBL 27-45, IT WAS FOUND TO BE WITHIN ACCEPTABLE LIMITS. (K)
Part: DOUBLER — CORRODED (FS425, RBL39)
DURING A C-CHECK, CORROSION WAS FOUND ON THE DOUBLER AT FS425, RBL 39. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE`S DETERMINATION OF THE APPROPRIATE CORRECTIVE ACTION. (K)
Part: DOUBLER — CORRODED (BS 513-517)
DURING A C-CHECK IN MCN, FOUND CORROSION ON THE DOUBLER AT FS 513-517, LBL 44-37. (M)
Part: FLOORBEAM — CRACKED (BS 280)
DURING A C-CHECK, THE FS280 FLOOR SUPPORT ANGLE, OB OF LBL9, AT ALTERNATE GEAR EXTENSION PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENEANCE REMOVED AND REPLACED THE FS280 FLOOR SUPPORT ANGLE, OB OF LBL9, AT ALTERNATE GEAR EXTENSION PULLEY, IAW REO 601R-53-11-138. (K)
Part: BULKHEAD — CRACKED (BS 280)
DURING A C-CHECK, THE FS 280 BULKHEAD, OB OF LBL 9 AND RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 BULKHEAD, OB OF LBL9 AND RBL 9, IAW EO 600-53-O123. (K)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
DURING A C-CHECK, THE FLOOR SUPPORT STRINGER, AT THE PASSENGER DOOR, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE FLOOR SUPPORT STRINGER IAW SRM 51-42-00, AND REPLACED THE FLOOR SUPPORT STRINGER IAW SRM 51-41-13 AND 51-42-06. (K)
Part: CLIP — CRACKED (FUSELAGE)
DURING A C-CHECK, THE AEB PRESSURE BULKHEAD LT AND RT SIDE CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AEB PRESSURE BULKHEAD LT AND RT SIDE CLIPS IAW SRM. (K)
Part: BULKHEAD — CRACKED (BS 202)
DURING A C-CHECK, THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. THE MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)
Part: BULKHEAD — CRACKED (FUSELAGE)
DURING C-CHECK, THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, IAW REO. (K)
Part: DOUBLER — CRACKED (FUSELAGE)
DURING A C-CHECK, THE FORWARD RT SIDE 718 DOUBLER, UNDER THE RADIUS BLOCK, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD RT SIDE 718 DOUBLER, UNDER THE RADIUS BLOCK, IAW EO 600-53-0066. (K)
2005
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
DURING AN OVERNIGHT CHECK IN VPS, THE EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 4. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS ON THE RT SIDE FROM ROW 6 TO THE GALLEY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIPS FROM ROW 2 TO 5. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)
Part: STEP — DEBONDED (PAX DOOR)
FLT 4638 - DURING A GROUND INSPECTION IN CVG THE SIDE ATTACH ROD TO THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND DISCONNECTED. MAINTENANCE FOUND THE BOTTOM STEP INSERTS DISBONDED FROM THE SIDE ATTACH ROD AND REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: SELECTOR VALVE — MALFUNCTIONED (MLG)
DURING CLIMB-OUT FROM TYS-ATL, UPON GEAR RETRACTION, THE CREW RECEIVED A RED GEAR DISAGREE WARNING MESSAGE FOR BOTH MAIN LANDING GEAR, MLG. CONCURRENTLY, THE NOSE GEAR FAILED TO EXTEND AND SUBSEQUENTLY EXTENDED AFTER THE CREW PERFORMED THE GEAR DOWN DISAGREE CHECKLIST. UPON COMPLETION OF THE REMAINING QRH ITEMS, THE DECISION WAS MADE TO CONTINUE THE FLIGHT TO ATL AND AN EMERGENCY WAS DECLARED. THE APPROACH AND LANDING IN ATL WERE MADE SAFELY. MAINTENANCE REMOVED AND REPLACED THE MLG SELECTOR VALVE AND BYPASS RUN AROUND VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: RESERVOIR — MALFUNCTIONED (NR 3 HYD SYS)
DURING TAKEOFF FROM ALT-GPT, UPON RAISING THE GEAR A GEAR UP DISAGREE MESSAGE WAS RECEIVED. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. EMERGENCY EQUIPMENT WAS ON STANDBY AS A PRECAUTION. MAINTENANCE REMOVED AND REPLACED THE NR 3 HYDRAULIC RESERVOIR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: STEP — BROKEN (PAX DOOR)
FLT 4287 - DURING A GROUND INSPECTION IN FWA, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2004
Part: PANEL — CRACKED (LEFT WING)
DURING A C-CHECK IN MCN, THE LEFT WING LOWER AFT PANEL AT WS 148.019 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT WING LOWER AFT PANEL AT WS 148.019 IAW ASA EO 600-57-0134. (M)
Part: RIB — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 IAW ASA EO 600-57-039A. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING A (C) CHECK, THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS559 + 32 TO FS 559 + 80 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS 559 +80.
Part: CLIP — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 IAW ASA EO 600-53-0098. (M)
Part: HANDLE — CRACKED (E/E BAY DOOR)
DURING (C) CHECK, THE AVIONICS BAY DOOR HANDLE CUP AROUND THE SUPPORT SHAFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS BAY DOOR HANDLE ASSEMBLY.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)
Part: SILL — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589. (M)
Part: CLIP — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280. (M)
Part: LIGHT — CRACKED (GALLEY)
DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT COVER IN THE GALLEY BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE GALLEY BY THE SERVICE DOOR. (M)
Part: COVER — MISSING (EMERGENCY LIGHT)
DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT COVER AT THE CABIN ENTRANCE WAS FOUND MISSING. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE CABIN ENTRANCE. (M)
Part: FRAME — CRACKED (FUSELAGE)
DURING A C-CHECK IN MCN, THE LEFT FRAME FS 718, STRINGER 10-11 AND DOUBLER WEAR FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT FRAME FS 718, STRINGER 10-11 AND DOUBLER IAW ASA EO 600-53-0066. (M)
Part: STEP — CRACKED (PAX DOOR)
DURING A C-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW SRM 51-73-00.
Part: COVER — DAMAGED (CABIN)
FLT 4413 - DURING A GROUND INSPECTION IN ATL, THE REAR EMERGENCY FLOOR LIGHT STRIP AND COVER WERE FOUND DAMAGED. MAINTENANCE RECONNECTED THE REAR EMERGENCY FLOOR LIGHT STRIP AND REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT COVER (P/N 5835-1). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2003
Part: ACM — ODOR (AIR CON SYS)
FLT 4441 - DURING CLIMB-OUT FROM PFN-ATL, THE CREW NOTICED A STRONG OIL ODOR FROM THE AIR CONDITIONING SYSTEM. THE ODOR WAS ALSO NOTICED DURING THE FLIGHT AT LOW AND IDLE POWER SETTINGS. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHING AND ALSO THE LEFT AND RIGHT COALESCER BAGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: SIGN — MISSING (CABIN)
DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT SIGN AT ROW 1 A/B WAS FOUND MISSING. MAINTENANCE INSTALLED AN EMERGENCY EXIT SIGN AT ROW 1 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: POWER SUPPLY — DISCHARGED (CABIN)
FLT 4784 - DURING A GROUND INSPECTION IN ATL, THE NR 1 AND 2 EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: SIGN — INOPERATIVE (CABIN)
FLT 4784 - DURING A GROUND INSPECTION IN ATL, AN EMERGENCY FLOOR LIGHT STRIP, SERVICE AND PASSENGER DOOR EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
FLT 4784 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP AT ROW TWO WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW TWO. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: STEP — CRACKED (PAX DOOR)
DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG DOOR)
FLT 4460 - DURING CLIMB-OUT FROM DFW-LEX, AT APPROXIMATELY 27,000 FEET THE CREW RECEIVED A NOSE DOOR OPEN WARNING MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE MESSAGE EXTINGUISHED WHEN THE GEAR WAS DOWN AND LOCKED. THE AIRCRAFT DIVERTED TO XNA, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT NOSE DOOR PROXIMITY SENSOR. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
FLT 4437 - DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY FLOOR LIGHTING STRIP WAS FOUND TO HAVE A LOOSE CONNECTION. MAINTENANCE REMOVED AND REPLACED THE FORWARD FIRST SECTION EMERGENCY FLOOR LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2002
Part: WARNING SYSTEM — ACTIVATED (COCKPIT)
FLT 4403 - DURING CLIMB THROUGH 10,000 FEET FROM GRR-ATL, A RIGHT THRUST REVERSER UNLOCK MESSAGE OCCURRED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO GRR AND LANDED SAFELY. MAINTENANCE DEFERRED THE THRUST REVERSER SYSTEM IAW MEL NR 78-30-1. (M)
Part: LIGHT — CONTAMINATED (CABIN)
FLT 4542 - DURING GROUND INSPECTION IN GNV, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND WATER THROUGH OUT THE ENTIRE FLOOR STRIP AND DRIED IT UP. MAINTENANCE REMOVED AND REPLACED THE SECTION OF FLOOR TRACK LIGHTING BETWEEN ROWS 5 AND 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (EXTERIOR)
FLT 4787 - DURING SCHEDULED INSPECTION IN XNA, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE LEFT FORWARD EXTERIOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)