N158GJ
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.
126 reports on file, 2009-04-23 – 2019-12-22.
Part: SMOKE WARNING — FALSE ACTIVATION (AFT LAVATORY) · airframe 37,907 hrs · 25,865 cycles
SMOKE AFT LAV WARNING MESSAGE SHORTLY AFTER TAKEOFF, ACCOMPANIED BY STRONG SMOKE ODOR THROUGHOUT AIRCRAFT. COMPLIED WITH LAV SMOKE DETECTOR WARNING, OPS CHECK GOOD. INSPECTED LAV TRASH CAN, LIGHTS, AND ALL CABINETS. NO FAULTS FOUND, IAW AMM-26-16-00.
Part: FITTING — CRACKED (BS 280-295) · airframe 35,730 hrs · 24,422 cycles
PASSENGER DOOR LINTEL IS CRACKED AT STRINGER 3L BETWEEN FS 280 & FS 295. CORRECTIVE ACTION: REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 670-53-21-493 REV. D DATED 2015-07-10 AND IAW BOMBARDIER SB 670BA-53-040 REV. C DATED SEP 20/2012.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 35,730 hrs · 24,422 cycles
VERTICAL STAB RT AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO C700-55MR-005-0.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 35,730 hrs · 24,422 cycles
VERTICAL STAB LT AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO C700-55MR-001-0.
Part: HOUSING — GOUGED (SERVICE DOOR) · airframe 35,730 hrs · 24,422 cycles
SERVICE DOOR HANDLE GOUGED. REMOVED AND REPLACED SERVICE DOOR HANDLE HOUSING (PN:133107-3) IAW SRM 51-42-21, 51-42-06, 51-77-00, 51-40-11, AND 51-25-16
Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,730 hrs · 24,422 cycles
STRINGER 26R CORRODED OUT OF LIMITS BETWEEN FRAME STATIONS 333 AND 364 IAW SRM 53-21-03. REPLACED STRINGER 26R BETWEEN FRAME STATIONS 333 AND 364 IAW SRM 51-40-11, 51-25-16, 51-42-06, 51-21-11.
Part: RETAINER — CORRODED (E&E DOOR) · airframe 35,730 hrs · 24,422 cycles
MAIN AVIONICS DOOR SEAL RETAINERS CORRODED. REPLACED MAIN AVIONICS DOOR SEAL RETAINERS IAW SRM 51-20-06, 51-42-06, 51-40-11, 51-42-10.
Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 35,730 hrs · 24,422 cycles
JB-6 MOUNTING BRACKET CRACKED. CORRECTIVE ACTION: REPLACED JB-6 MOUNT BRACKET IAW SRM 51-42-06 AND 51-40-11.
Part: SUPPORT BRACKET — CRACKED (LE SLAT) · airframe 35,730 hrs · 24,422 cycles
LEFT WING SLAT TRACK 1-3 CANISTER SUPPORT BRACKET CRACKED. CORRECTIVE ACTION: REPAIRED SLACK TRACK 1-3 CANISTER BRACKET IAW REO 670-57-42-577 DATED 2016-12-02 AND NDTM PART 1 51-20-006 AND SRM 51-26-00,
Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 35,730 hrs · 24,422 cycles
RIGHT HAND LOWER THRUST REVERSER INBOARD STANDOFF BRACKET CRACKED. REPLACED RIGHT HAND THRUST REVERSER INBOARD STANDOFF BRACKET IAW SRM 51-42-13, 51-42-24 AND 51-40-11.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,730 hrs · 24,422 cycles
LT FS 280 BULKHEAD I/B STIFFENER CRACKED. REMOVED AND REPLACED CRACKED STIFFENER AT LT FS 280 BULKHEAD I/B IAW SRM 51-42-06.
Part: SKIN — DENTED (BS 1000-1015) · airframe 35,730 hrs · 24,422 cycles
AFT FUSELAGE LH SIDE BETWEEN FS 1000.00 AND FS 1015.00 AT STGR 18L THERE IS A DENT(UNDER PROTECTOR PLATE) AND STGR 18L IS BENT. CORRECTIVE ACTION: REMOVED DAMAGED STGR 18L. DRESSED FUSELAGE SKIN TO NORMAL CONFIGURATION. NO DAMAGE NOTED TO SKIT. PERFORMED DNT ON SKIN, NO DAMAGE FOUND. INSTALLED REPAIR SPLICE AND NEW STGR 18LH. REMOVED DAMAGED FRAMES AT FACTORY SPLICE AND INSTALLED NEW FRAME SECTIONS AND NEW FRAME SPLICES AT FS 1000.00 AND FS 1015.00. RESTORED FINISH AT STGR 18L IAW BOMBARDIER CRJ700 REO 670-51-00-085 REV A 2017-0-03, SRM 53-61-03, 53-61-06, 51-42-21, REO 670-53-61-1520 2019-02-08, SRM 51-25-06, 51-42-06, AMM 20-70-00, NDTM 51-20-006.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,730 hrs · 24,422 cycles
QUARTER TURN ANGLE, ATTACHED TO FS 280 BEAM, CRACKED. REMOVED AND REPLACED CRACKED 1/4 TURN ANGLE ATTACHED TO FS 280 BEAM IAW SRM 51-42-06.
Part: PLATE — CRACKED (ZONE 200) · airframe 35,730 hrs · 24,422 cycles
FWD EQUIPMENT COMPARTMENT RT DOOR LATCH PLATE CRACKED. REMOVED AND REPLACED RT FWD EQUIPMENT BAY DOOR LATCH PLATE IAW SRM 51-42-06.
Earlier reports · 2009–2018 · 112 reports
2018
Part: LIGHT — INOPERATIVE (ROWS 15 & 21) · airframe 34,484 hrs · 23,654 cycles
TWO OVERHEAD EMERGENCY EXIT LIGHTS WERE INOPERATIVE, ROW 15 & 21.
Part: LIGHT — INOPERATIVE (ROW 11) · airframe 33,531 hrs · 23,063 cycles
CEILING EMERGENCY LIGHT AT ROW 11 INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOODLIGHT AT ROW 11 IAW MM 33-51-09. OPS CHECKED GOOD.
Part: COVER — BROKEN (PAX DOOR) · airframe 33,489 hrs · 23,037 cycles
WIRE HARNESS COVER BROKEN ON MAIN CABIN DOOR. REPAIRED THE WIRE HARNESS COVERING IAW ESPM 20-33-00.
Part: WEB — CORRODED (FUSELAGE) · airframe 15,235 hrs · 12,254 cycles
RT LOWER WEB CORRODED AT FS 280.00. REPAIRED RT LOWER WEB AT FS 280.00 IAW SRM 51-42-21, 51-42-06, 53-11-10 AND 51-25-16.
2017
Part: WARNING MESSAGE — FALSE ACTIVATION (SERVICE DOOR) · airframe 31,557 hrs · 21,566 cycles
SERVICE DOOR CAUTION. PERFORMED ADJUSTEMENT OF SERVICE DOOR IAW AMM 52-41-02. NO FAULTS FOUND.
Part: SEAL — LEAKING (ESCAPE HATCH) · airframe 31,113 hrs · 21,232 cycles
CREW ESCAPE HATCH IS LEAKING WATER. PERFORMED LUBRICATION OF CREW ESCAPE HATCH IAW AMM 12-20-52. NO FURTHER DEFECTS NOTED.
Part: WARNING MESSAGE — ILLUMINATED (SERVICE DOOR) · airframe 30,564 hrs · 20,816 cycles
SERVICE DOOR OUTER HANDEL CAUTION MESSAGE.
2016
Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 30,337 hrs · 20,639 cycles
EMER LIGHT ON STATUS MSG WITH SWITCH IN ARMED POS. PERFORMED CO RESET. OPS CHECK IAW AMM 33-51-00, OPS CHECK GOOD.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,127 hrs · 20,472 cycles
FOUND A CRACK ON THE LEFT OF THE BS 280 FLOORBEAM.
Part: ESCAPE HATCH — NOT SEATED (COCKPIT) · airframe 29,596 hrs · 20,092 cycles
WATER LEAKING FROM CREW ESCAPE HATCH. INSPECTED CREW ESCAPE HATCH AND RESEATED IAW AMM 52-22-00, NO FURTHER LEAKS DETECTED.
Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 29,429 hrs · 19,978 cycles
PASSENGER DOOR WARNING, ADJUSTED PASSENGER DOOR SENSOR IAW AMM 52-70-04, OPS CHECK GOOD AT THIS TIME AND EICAS DOOR INDICATION IS GREEN.
Part: ESCAPE HATCH — DIRTY (COCKPIT) · airframe 29,038 hrs · 19,365 cycles
CREW ESCAPE HATCH LEAKING WATER. CLEANED & LUBED CREW ESCAPE HATCH IAW AMM 12-20-52. RE-INSTALLED DOOR IAW AMM 52-22-00. LEAK CHECKED GOOD. NO DEFECTS NOTED OR LEAKS.
Part: WHEEL — MALFUNCTIONED (PAX DOOR) · airframe 28,319 hrs · 19,201 cycles
RAMP REPORTS PAX DOOR SUPPORT WHEEL FAILED TO DEPLOY. PERFORMED ZONAL INSPECTION OF THE PAX DOOR FOR DAMAGE. PERFORMED OPERATIONS CHECK OF THE PAX DOOR IAW AMM 52-11-00. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: SENSOR — DEFECTIVE (PAX DOOR) · airframe 28,253 hrs · 19,153 cycles
DURING CRUISE FLIGHT, HEARD A POP SOUND WITH PAX DOOR WARNING INDICATION WITH PROX SYS M FAULT STATUS FAULT 1 MSG. ALSO AN ELEC BURNING SMELL & AN AFT CARGO DOOR CAUTION. TROUBLE SHOT & FOUND MAIN PAX DOOR SENSOR PX101 TO BE BAD IAW FIM 52-70-04, TRANSFERRED FAULT TO DISC NR 3M. FAULT REMAINS OPEN.
Part: STEP — SHEARED (PAX DOOR) · airframe 28,179 hrs · 19,103 cycles
FOLDING STEP RETRACTION ARE SHEARED OFF PAX DOOR. R & R FOLDING STEP IAW AMM 52-11-04 & RETRACTION RON IAW AMM 52-11-05.
2015
Part: ESCAPE HATCH — LEAKING (COCKPIT) · airframe 27,917 hrs · 18,917 cycles
CREW ESCAPE HATCH LEAKING. REMOVED WATER AS REQUIRED. ACFT OK FOR SERVICE.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,571 hrs · 18,644 cycles
EMERGENCY EXIT FLOOR LIGHT 18D INOPERATIVE. R & R POWER SUPPLY IAW AMM 33-51-17. OPERATIONS CHECKED GOOD.
Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 27,566 hrs · 18,640 cycles
EMERGENCY LIGHTS ON STATUS MSG ON & OFF IN FLIGHT. PERFORMED OPERATIONS CHECK OF EMER LIGHTS IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.
Part: ESCAPE HATCH — LACK OF LUBE (COCKPIT) · airframe 26,939 hrs · 18,197 cycles
CREW ESCAPE HATCH LEAKS EXCESSIVE. LUBED CREW ESCAPE HATCH IAW AMM 52-22-00.
Part: CABLE — BROKEN (PAX DOOR) · airframe 26,796 hrs · 18,100 cycles
PASSENGER DOOR SUPPORT WHEEL CABLE BROKEN. R & R PAX DOOR CABLE IAW AMM 52-11-13. OPERATIONS CHECKED GOOD.
Part: LENS — OUT OF POSITION (CABIN) · airframe 25,980 hrs · 17,532 cycles
EMERGENCY EXIT FLOOR LIGHT COVER MISSING AT SERVICE DOOR. FOUND EXIT DOOR LIGHT LENS COVER. INSPECTED LENS & FOUND EXIT PLACARD MISSING. DEFERRED ON NEF 25-100-12 CAT 1.
Part: ESCAPE HATCH — DIRTY (COCKPIT) · airframe 25,623 hrs · 17,300 cycles
FLIGHT DECK ESCAPE HATCH LEAKING FLUID. CLEANED & LUBED ESCAPE HATCH, DRAINED DE-ICE FLUID. OPERATIONS CHECKED GOOD.
2014
Part: PIN — NOT SEATED (PAX DOOR) · airframe 25,272 hrs · 17,072 cycles
PROX SWITCH PX 23, PAX DOOR UPPER LOCK, FOUND OPEN. FOUND PSEU CONNECTOR P363 PIN PUSHED IN. RESEATED PUSHED PIN IAW ESPM 20-26-00. OPERATIONS CHECK OF THE PAX DOOR IS GOOD IAW AMM 52-11-00.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 25,272 hrs · 17,072 cycles
LOWER T CAS ANTENNA MOUNT CHANNEL CORRODED. R & R T CAS CHANNEL IAW SRM 51-42-06. WORK ORDER 80258 WORK CARD 1088.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,272 hrs · 17,072 cycles
FLOOR SUPPORT ANGLE AFT SIDE OF FS 280 CORRODED. R & R SUPPORT ANGLE IAW SRM 51-42-06. WORK ORDER 80258 WORK CARD 1087.
Part: PROXIMITY SWITCH — FAILED (PAX DOOR) · airframe 25,272 hrs · 17,072 cycles
PASSENGER DOOR FAILED OPERATIONS CHECK. DOOR INDICATION ON EICAS TURNS RED AT FIRST HANDLE DETENT, NEVER TURNED AMBER. R & R PAX DOOR PROX SWITCH PX 107 IAW AMM 52-70-04. OPERATIONS CHECKED GOOD. WORK ORDER 80258 WORK CARD 8040.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,272 hrs · 17,072 cycles
AFT WING TO BODY FAIRINGS SUPPORT WEB JOINT ANGLE AT FS 953 CORRODED. R & R ANGLE IAW SRM 51-42-06. WORK ORDER 80258 WORK CARD 1082.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,272 hrs · 17,072 cycles
FLOOR SUPPORT, QUARTER TURN ANGLE FOR LIBRARY BOX, ON FS 280 FLOORBEAM CORRODED. R & R SUPPORT IAW SRM 51-42-06. WORK ORDER 80258 WORK CARD 1068.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 25,272 hrs · 17,072 cycles
FLOORBEAM AT FS 280 IS CRACKED. R & R FLOORBEAM IAW SRM 53-11-41. WORK ORDER 80258 WORK CARD 1067.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,164 hrs · 17,007 cycles
AFT CEILING EMER LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-09.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,092 hrs · 16,951 cycles
RIGHT EMER DOOR CAUTION MSG. DEFERRED IAW MEL 52-70-03 CAT C.
Part: CONNECTOR — DIRTY (PAX DOOR) · airframe 24,755 hrs · 16,730 cycles
PAX DOOR LATCH CAUTION MSG. CLEANED & SECURED PAX DOOR ELEC CONNECTOR. PERFORMED OPERATIONS CHECK OF DOOR WARNING SYS IAW AMM 52-70-04. NO MSG NOTED.
Part: DOOR — OPEN (GROUND POWER) · airframe 24,459 hrs · 16,537 cycles
GPU DOOR LT OPEN. PERFORMED EXTERNAL ZONAL INSPECTION OF GPU DOOR & SURROUNDING AREA. DOOR OPENS & CLOSES PROPERLY. NO DEFECTS NOTED IAW AMM 05-21-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,440 hrs · 16,523 cycles
EMERGENCY EXIT LIGHT INOPERATIVE. RE-LAMPED EMER EXIT LIGHT IAW AMM 20-21-00. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 24,325 hrs · 16,449 cycles
RIGHT EMER EXIT DOOR MSG INTERMITTENT. DEFERRED RT EMER EXIT DOOR INDICATION IAW MEL 52-70-03 CAT C.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 24,071 hrs · 16,291 cycles
EMERGENCY LIGHTS ILLUMINATE IN THE ARM POSITION. PERFORMED OPERATIONS CHECK OF ELEC LIGHTS SYS IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
Part: BATTERY — MALFUNCTIONED (CABIN) · airframe 23,975 hrs · 16,231 cycles
EMERGENCY LIGHTS COME ON IN ARM POSITION. RESET BATTERY & PERFORMED OPERATIONS CHECK OF EMERGENCY LIGHT IAW AMM 33-51-17, OPERATIONS CHECKED GOOD AT THIS TIME.
Part: EPSU — MALFUNCTIONED (CABIN) · airframe 23,880 hrs · 16,174 cycles
EMERGENCY LIGHTS TURN ON IN THE ARMED POSITION. RERACKED EPSUS IAW AMM 33-51-14, OPERATIONS CHECKED GOOD AT THIS TIME.
Part: PLACARD — WORN (PAX DOOR) · airframe 23,706 hrs · 16,058 cycles
PAX DOOR OPEN & EXIT PLACARDS WORN. R & R PAX DOOR OPEN & CLOSED EXIT PLACARDS IAW AMM 20-60-04.
Part: SEAL — DIRTY (ESCAPE HATCH) · airframe 23,368 hrs · 16,052 cycles
CREW ESCAPE HATCH LEAKING. CLEANED & LUBRICATED HATCH SEAL IAW AMM 52-22-00.
Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 23,668 hrs · 16,031 cycles
FOUND CRACK ON TOP OF PAX DOOR BELOW TOP STEP. REPAIRED CRACK DAMAGE IAW SRM 52-11-04.
Part: ESCAPE HATCH — DIRTY (COCKPIT) · airframe 23,580 hrs · 15,971 cycles
ESCAPE HATCH LEAKING. OPENED COCKPIT CREW EMERGENCY HATCH & CLEANED SOME DEBRIS & INSPECTED IAW AMM 52-22-00. NO FURTHER LEAKS DETECTED AT THIS TIME.
Part: LENS — MISSING (CABIN) · airframe 23,573 hrs · 15,967 cycles
FORWARD EXIT FLOOD LIGHT LENS COVER MISSING. DEFERRED FWD EXIT EMERGENCY LENS COVER IAW MEL 33-51-01C CAT C.
Part: DOOR SEAL — DIRTY (ESCAPE HATCH) · airframe 23,518 hrs · 15,935 cycles
CREW ESCAPE HATCH LEAKING. CLEANED & LUBED COCKPIT CREW ESCAPE HATCH SEAL IAW AMM 52-22-00. NO FURTHER LEAKS NOTED AT THIS TIME.
Part: SEAL — DIRTY (ESCAPE HATCH) · airframe 23,507 hrs · 15,929 cycles
COCKPIT ESCAPE HATCH LEAKING. CLEANED DEBRIS & LUBED ESCAPE HATCH SEAL IAW AMM 12-20-52, OPERATIONS CHECKED GOOD, NO LEAKS.
Part: ESCAPE HATCH — LEAKING (COCKPIT) · airframe 23,469 hrs · 15,903 cycles
CREW ESCAPE HATCH LEAKING. CLEANED & LUBED CREW ESCAPE HATCH IAW AMM 12-20-52.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,453 hrs · 15,893 cycles
RIGHT EMERGENCY DOOR CAUTION MSG. REMOVED RT EMERGENCY DOOR, INSPECTED DOOR, NO DEFECTS NOTED. REINSTALLED RT EMERGENCY DOOR IAW AMM 52-21-00.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 23,372 hrs · 15,841 cycles
EMERGENCY LIGHTS STAY ON IN THE ARMED POSITION, AFTER POWERING OFF THE ACFT SYS. OPERATIONS CHECKED NORMAL IAW CRJ700 33-50-00.
Part: ESCAPE HATCH — DIRTY (COCKPIT) · airframe 23,259 hrs · 15,772 cycles
WATER DRIPPING THROUGH CREW ESCAPE ON FIRST OFFICER`S SIDE. OPENED & CLEANED CREW ESCAPE HATCH SEAT, LUBED SEAL & REINSTALLED HATCH IAW CRJ700 AMM 112-20-52, NO LEAK AT THIS TIME.
2013
Part: ESCAPE HATCH — LEAKING (COCKPIT) · airframe 22,679 hrs · 15,412 cycles
ESCAPE HATCH LEAKING. INSPECTED & PERFORMED OPERATIONS ON OVERHEAD FLIGHT DECK ESCAPE HATCH IAW CRJ700 AMM 52-22-00. OPERATIONS & LEAK CHECKED GOOD AT THIS TIME.
Part: MONITOR — FAULTY (BRAKE SYSTEM) · airframe 22,577 hrs · 15,236 cycles
NR 1 BRAKE OVERHEAT IN FLIGHT. DEFERRED NR 1 EICAS BRAKE TEMP MONITOR ON DMI 30452000, IAW MEL 32-46-01D CAT C.
Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 22,134 hrs · 15,045 cycles
EMERGENCY LIGHTS IN CABIN COMES ON MOMENTARILY AND THEN GOES OUT. PERFORMED OP'S CHECK OF EMERGENCY LIGHT IAW AMM 33-51-17. OK FOR SERVICE AT THIS TIME.
Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 21,020 hrs · 14,321 cycles
OVERWING EMERGENCY EXIT HANDLE COVER WON'T STAY CLOSED. INSTALLED HOOK AND LOOP ON RT EMERGENCY HATCH HANDLE COVER IAW AMM 25-26-04.
Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 21,020 hrs · 14,321 cycles
RT OVERWING EXIT HANDLE COVER WILL NOT STAY IN PLACE. PLACED HANDLE COVER.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 20,332 hrs · 13,383 cycles
ON TAKEOFF ROLL AT 80 KIAS, RECEIVED A MASTER CAUTION WARNING LIGHT, "SMOKE AFT LAV" & "FIRE SYSTEM FAULT" STATUS MESSAGE. INSPECTED LAV FOR EVIDENCE OF SMOKE. NO EVIDENCE FOUND. PERFORMED OP'S CHECK ON LAV SMOKE DETECTOR SYS IAW AMM 26-10-00. OP'S CHECK GOOD AT THIS TIME.
Part: STARTER — MALFUNCTIONED · airframe 20,310 hrs · 13,850 cycles
NO STARTER CUTOUT, MASTER CAUTION IN FLIGHT. INSPECTED STARTER, NO DEFECTS NOTED, PERFORMED 3 ENG STARTS, OPS CHECK GOOD IAW AMM 71-00-00.
Part: SEAL — DIRTY (ESCAPE HATCH) · airframe 20,265 hrs · 13,819 cycles
CREW ESCAPE HATCH SPILLING WATER ONTO UPPER PEDESTAL. CLEANED, INSPECTED AND LUBED SEAL, NO DEFECTS NOTED IAW AMM 52-22-07.
Part: INTERCOSTAL — CORRODED (BS 349-364 S27) · airframe 20,205 hrs · 13,774 cycles
STRINGER 27 INTERCOSTAL AT FS 349-364 CORRODED. R & R STRINGER 27 INTERCOSTAL, IAW SRM 51-42-06 AT FS 349-364.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,205 hrs · 13,774 cycles
PAX DOOR MID CAP ANGLE CORRODED. R & R PAX DOOR MID CAP ANGLE IAW SRM 51-42-13 & SRM 51-40-11.
Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 20,205 hrs · 13,774 cycles
AFT COCKPIT FLOOR SUPPORT ANGLE CORRODED. R & R ANGLE IAW SRM 51-42-06.
Part: SKIN — CHAFED (BS 696-985) · airframe 20,205 hrs · 13,774 cycles
FUSELAGE SKIN HAS CHAFING DAMAGE AT FS 696 TO 985 AT STRINGER 27. CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION OF THE REMAINING AREA IAW MTM 51-20-006, NO DEFECTS FOUND. FABRICATED AND INSTALLED DOUBLER IAW 670-53-61-935.
Part: STEP — OUT OF RIG (PAX DOOR) · airframe 20,205 hrs · 13,774 cycles
PAX DOOR LOWER STEP OUT OF RIG. ADJUSTED LOWER PAX DOOR STEP IAW AMM 52-11-04, OP'S CHECKED GOOD AT THIS TIME.
2012
Part: WIRE — DAMAGED (DOOR WARNING) · airframe 19,484 hrs · 13,295 cycles
PROXIMITY SYS FAULT 2 STATUS MESSAGE. REPAIRED WIRES ON PAX DOOR INDICATION HARNESS. ALSO R & R CONNECTOR A268P1 IAW ESPM 20-26-0 PO'S CHECK GOOD AT THIS TIME AMM 52-70-00, NO DEFECTS NOTED.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 19,466 hrs · 13,281 cycles
PAX DOOR PROXIMITY SYS 2 STATUS MESSAGE. OP'S CHECK PERFORMED IAW AMM 52-70-00, NO MESSAGES NOTED AT THIS TIME.
Part: PSEU — MALFUNCTIONED (PAX DOOR) · airframe 19,389 hrs · 13,225 cycles
PAX DOOR MASTER WARNING MESSAGE ON WHEN CLOSED. R & R PSEU OP'S CHECKED GOOD AT THIS TIME IAW AMM 32-61-01.
Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 19,389 hrs · 13,225 cycles
PAX DOOR CAUTION MESSAGE AND PASSENGER DOOR SHOWS RED ON DOOR SYNOPTIC PAGE WHEN PAX DOOR IS CLOSED. COMPLIED WITH PAX DOOR WARNING SYS TEST IAW AMM 52-11-00 & NO FURTHER DEFECTS NOTED AT THIS TIME.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 19,389 hrs · 13,225 cycles
PAX DOOR MASTER WARNING ON TAXI. INTERMITTENTLY DOOR SHOWS RED ON SYNOPTIC PAGE WITH ALL GREEN PINS ALIGNED. COMPLIED WITH PAX DOOR WARNING IGNITION TEST IAW AMM 52-11-00 AND 52-70-04, NO FAULTS NOTED AT THIS TIME.
Part: WARNING SYSTEM — FALSE ACTIVATION (PAX DOOR) · airframe 19,376 hrs · 13,218 cycles
MAIN PAX DOOR SHOWS OPEN WHEN DOOR IS CLOSED. RESET SYS, OP'S CHECKED GOOD IAW AMM 52-70-04.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,298 hrs · 13,171 cycles
EMERGENCY LIGHT IN ROW 15 ON CEILING OUT. R & R EMERGENCY LIGHT BULB AT ROW 15 IAW AMM 33-51-09. OP'S CHECK GOOD AT THIS TIME.
Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 18,869 hrs · 12,887 cycles
PROXIMITY SYSTEM FAULT 2 STATUS MESSAGE- DETERMINED PROXIMITY 2 MESSAGE FROM PAX DOOR. VERIFIED PAX DOOR CLOSES AND LOCKS. ACFT SAFE FOR ONE TIME FERRY IAW AMM 52-11-00.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,666 hrs · 12,750 cycles
EMERGENCY CEILING FLOOD LIGHT OUT AT ROW 15. RELAMPED EMERGENCY FLOOD LIGHT IAW AMM 33-51-07.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,195 hrs · 12,431 cycles
EMERGENCY EXIT LIGHT ABOVE ROW 15 IS BURNED OUT. R & R EXIT LIGHT BULB AT ROW 15 IAW AMM 33-51-09, OPS CHECKED GOOD.
Part: CABLE ASSY — BROKEN (PAX DOOR) · airframe 18,195 hrs · 12,431 cycles
PASSEMGER DOOR BOTTOM CABLE ASSY BROKEN. R & R CABLE ASSY IAW AMM 52-11-13.
Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 18,178 hrs · 12,421 cycles
PAX DOOR OUTER HANDLE CAUTION MESSAGE.
Part: PIN — MISSING (PAX DOOR) · airframe 17,702 hrs · 12,104 cycles
FORWARD PASSENGER DOOR HAND RAIL PIN MISSING. DEFERRED FORWARD HAND RAIL PIN IAW MEL 52-11-05, CAT C.
Part: BULB — OUT OF POSITION (EMERGENCY LIGHT) · airframe 17,467 hrs · 11,966 cycles
TWO EMERGENCY LIGHTS ADJACENT TO EACH OTHER INOPERATIVE, ROW 10 AND 15. REPOSITIONED LIGHT BULB AT ROW 10 AND OPS CHECKED GOOD IAW AMM 33-51-00.
Part: SEAL — DIRTY (ESCAPE HATCH) · airframe 17,452 hrs · 11,958 cycles
CREW ESCAPE HATCH LEAKING WATER ON THE LOWER PANEL. CLEANED ESCAPE HATCH SEAL AND RESECURED HATCH IAW AMM 52-22-00 NO FUTHER LEAKS NOTED. DRIED UP STANDING WATER AS REQUIRED. POWERED ACFT, NO DEFECTS NOTED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,428 hrs · 11,943 cycles
CEILING EMERGENCY LIGHT BETWEEN 9 AND 10 BURNED OUT. RELAMPED OVERHEAD EMER LIGHT IAW AMM 33-51-09.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,155 hrs · 11,772 cycles
EMERGENCY LIGHT INOPERATIVE ROW 13. R & R EMERGENCY LIGHT IAW AMM 33-31-09.
Part: WARNING MESSAGE — FALSE INDICATION · airframe 16,709 hrs · 11,491 cycles
EMERGENCY LIGHTS ON STATUS MESSAGE. INSPECTED EMERGENCY LIGHT FOUND NO MESSAGE AND OPS CHECKED EMERGENCY LIGHTS SYS IAW AMM 33-51-00. OPS CHECKED GOOD AT THIS TIME.
Part: HAND RAIL — DAMAGED (PAX DOOR) · airframe 16,551 hrs · 11,388 cycles
METAL BRACKET CAME OFF MAIN ENTRANCE DOOR LT PIN SHAFT. INSPECTED AND FOUND FORWARD HANDRAIL SPRING CLIP MISSING. FOUND TO BE WITH IN LIMITS IAW REO 670-52-11-027 ENTERED ON CARRY OVER 1801.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 15,959 hrs · 11,015 cycles
LT OVERWING EMERGENCY LIGHT COVER CRACKING. R & R EMERGENCY LIGHT COVER IAW AMM 20-21-00.
Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 15,950 hrs · 11,009 cycles
RT OVERWING EMERGENCY EXIT DOOR INNER HANDLE COVER LOOSE. RESECURED PLASTIC GUARD AS REQUIRED.
Part: WIRE — BROKEN (DOOR SENSOR) · airframe 15,944 hrs · 11,005 cycles
PASSSENGER DOOR PROX SYSTEM FAULT 2. FOUND BROKEN WIRE TO PX47 REPAIRED BROKEN WIRE TO PX47 IAW FIM 52-70-04.
Part: DOOR — FAILED (MAIN PAX) · airframe 15,922 hrs · 10,993 cycles
PASSENGER DOOR FREE FALLS. DEFERRED PASSENGER DOOR POWER ASST ON DMI 26373 IAW MEL 52-11-01, CAT C.
Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 15,883 hrs · 10,971 cycles
DIVERTED, LOSS OF HYD FLUID SYS 3 INFLIGHT. REPAIRED NR 3 SYS LINE IAW AMM 20-30-00. OPS AND LEAK CHECK GOOD.
Part: WIRE — BROKEN (PROX SENSOR) · airframe 15,697 hrs · 10,850 cycles
PROX SYS 2 FAILED. LOCATED BROKEN WIRE IN SYS AND SPLICED IT IAW ESPM 20-44-11. PERFORMED OPS CHECK OF PAX DOOR SYSTEM IAW AMM 52-70-04. OPS CHECKED GOOD.
Part: CABLE — BROKEN (PAX DOOR) · airframe 15,386 hrs · 10,660 cycles
DURING PRE-FLIGHT WALKAROUND, FOUND PASSENGER DOOR VENT FLAP CABLE BROKEN. R & R DOOR ICE BREAKER CABLE IAW AMM 52-11-15.
Part: PROXIMITY SWITCH — MALFUNCTIONED (PAX DOOR) · airframe 14,797 hrs · 10,301 cycles
PASSENGER DOOR OUTER HANDLE CAUTION MSG CAME ON THEN OFF ON ARRIVAL WITH A PROX SYS 2, STATUS MSG. R & R PROX SWITCH PX107 ON OUTER PASSENGER DOOR HANDLE IAW AMM 52-70-04. OPS CHECKED GOOD AT THIS TIME IAW AMM 52-11-00. NO MESSAGE NOTED AT THIS TIME.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 14,797 hrs · 10,301 cycles
BACKLIGHT FOR PASSENGER EMERGENCY EXIT SIGN/LIGHT PANEL IN NOT WORKING. R & R PASSENGER SIGN/EMERGENCY LIGHT PANEL, CLEANED AND RESECURED ELECTRICAL CONNECTOR. REINSTALLED PANEL IAW AMM 33-24-07, OPS CHECKED GOOD AT THIS TIME.
Part: FITTING — CORRODED (BS 310) · airframe 14,557 hrs · 10,159 cycles
FWD FUSELAGE CLOSER FITTING, FS 310.00 AT LBL 18 CORRODED. R & R FWD FUSELAGE CLOSER FITTING AT FS 310.00 AND LBL 18 AS REQUIRED IAW SRM 51-42-20-001.
Part: FITTING — CORRODED (BS 286) · airframe 14,557 hrs · 10,159 cycles
GALLEY FITTING FS 286, RBL 18 CORRODED. R & R GALLEY FITTING FS 286, RBL 18 IAW SRM 51-42-11.
Part: ANGLE — CORRODED (BS 280 BULKHEAD) · airframe 14,557 hrs · 10,159 cycles
STA 280.00 BULKHEAD LWR ANGLE CORRODED RBL 37. FABRICATED AND INSTALLED ANGLE STA 280.00, RBL 37 IAW SRM 53-11-10.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,557 hrs · 10,159 cycles
FUS STA 280.00, FROM LBL 9 TO RBL 9 CORRODED FLOOR CHANNEL SUPPORT. REMOVED AND INSTALLED FLOOR ANGLE CHANNEL SUPPORT IAW SRM 51-42-06.
Part: SILL — CORRODED (ZONE 200) · airframe 14,557 hrs · 10,159 cycles
AFT CARGO BAY, DOOR FRAME LOWER SILL HAS EXFOLIATION CORROSION. AFT CARGO BAY DOOR FRAME LOWER SILL, R & R IAW SRM 53-61-23, HOLES IAW 51-40-11, RIVETS IAW 51-42-06, HI LOKS IAW 51-42-20, BLIND FASTENERS IAW 51-42-15, ALODINE IAW 51-21-16, PRIMER IAW 51-25-06, PAINT IAW 51-25-21, NUT PLATES IAW 51-45-00, AND SEALANT IAW 51-23-00.
Part: FLOOR SUPPORT — CORRODED (BS 316) · airframe 14,557 hrs · 10,159 cycles
FLOOR SUPPORT CLOSING ANGLE, FUS STA 316.00 CORRODED. REMOVED AND INSTALLED NEW CLOSING ANGLE FITTING IAW SRM 53-21-23 AND SRM 51-42-06.
Part: ANGLE — CORRODED (ZONE 100) · airframe 14,557 hrs · 10,159 cycles
FORWARD FUS SERVICE DOOR LOWER SECTION, MOUNTING ANGLE CORRODED. R & R ANGLE MOUNTING PN SH 670-31996-3, BATCH 106807 IAW ARM 53-21-23, SRM 51-42-06, SRM 51-42-02 AND SRM 51-23-00.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,557 hrs · 10,159 cycles
FUSELAGE STA 280.00 FLOORBEAM IS CORRODED. ACCOMPLISHED FLOORBEAM 280.00 REPLACEMENT-SPLICE REPAIR IAW REO 670-53-11-047-E.
Part: BULKHEAD — CORRODED (BS 280) · airframe 14,557 hrs · 10,159 cycles
FWD FUS LT BULKHEAD, FUS STA 280.00, LOWER WEB CORRODED. REMOVED AND INSTALLED FWD FUS LT BULKHEAD FS 280.00 LOWER WEB IAW SRM 53-11-10.
Part: FITTING — CORRODED (BS 295) · airframe 14,557 hrs · 10,159 cycles
GALLEY FITTING FS 295.00 AT RBL 4 CORRODED. R & R GALLEY FITTING FS 295.00 AT RBL 4 IAW SRM 51-42-21.
Part: FITTING — CORRODED (BS 316) · airframe 14,557 hrs · 10,159 cycles
GALLEY FITTING FUSELAGE STA 316.00 AT RBL 7 CORRODED. (FWD FUSELAGE). REMOVED GALLEY FITTING FUS STA 316.00, RBL 7, REMOVED NUTPLATE FROM OLD FITTING AND INSTALLED ON NEW FITTING. INSTALLED GALLEY FITTING FUS STA 316.00, RBL 7. APPLIED ALODINE, PRIMED AND PAINTED WHITE IAW SRM 51-42-20 AND SRM 51-21-16.
Part: ANGLE — CORRODED (ZONE 100) · airframe 14,557 hrs · 10,159 cycles
PAX ENTRY DOOR MID CAP ANGLE CORRODED. REMOVED AND INSTALLED NEW MID CAP ANGLE. PN SH670-31825-7 IAW SRM 53-21-23 AND SRM 51-41-02.
Part: FITTING — CORRODED (BS 289) · airframe 14,557 hrs · 10,159 cycles
CLOSET FITTING, FUS STA 289.00 AT LBL 18 IS CORRODED. R & R CLOSET FITTING IAW SRM 51-42-11.
Part: SILL — CORRODED (BS 295) · airframe 14,557 hrs · 10,159 cycles
FWD FUS LT SILL FUS STA 295.00 CORRODED. REMOVED SURFACE CORROSION WITIN LIMITS, ALODINE PRIME AND PAINT BLENDED AREA IAW SRM 51-21-06, 53-21-43, AND 53-21-45.
Part: ANGLE — CORRODED (ZONE 100) · airframe 14,557 hrs · 10,159 cycles
PAC ENTRY DOOR KICK PLATE ANGLE CORRODED. REMOVED AND INSTALLED NEW KICKPLATE ANGLE PN SH67031875-5, BATCH 12920.
Part: BULKHEAD — CORRODED (BS 280) · airframe 14,557 hrs · 10,159 cycles
FWD FUS RT BULKHEAD, FUS STA 280, LOWER WEB CORRODED. REMOVED AND INSTALLED FWD FUS RT BULKHEAD, FUS STA 280, LOWER WEB IAW SRM 53-11-10 AND REO 670-53-11-578.
2010
Part: COMPUTER — MALFUNCTIONED (FUEL QTY) · airframe 12,943 hrs · 9,065 cycles
FUEL CH 1/2 FAIL CAUTION MESSAGE IN FLIGHT. R & R FUEL QUANTITY GAUGING COMPUTER IAW AMM 28-41-22, OPS CHECK GOOD AT THIS TIME.
Part: AHRS — MALFUNCTIONED · airframe 12,929 hrs · 9,055 cycles
FO/STBY COMPASS HEADING DISAGREE BY 40-50 IN FLIGHT AFTER LANDING 174, 118, 111 ON GROUND RESPECTIVELY. SWAPPED AHRS FOR TROUBLESHOOTING AND PERFORMED OPS CHECK NO HEADING SPLIT NOTED IAW AMM 34-21-01.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,456 hrs · 8,732 cycles
EMERGENCY LIGHTS ON IN ARMED POSITION. PERFORMED OPS CHECK ON EMERGENCY LIGHT SYS PER AMM 33-51-00. OPS CHECK GOOD AT THIS TIME.
Part: GLOWSTRIP — MISSING (CABIN) · airframe 12,446 hrs · 8,726 cycles
PHOTOLUMINESCENT OVERWING MARKER CROSS SECTION BEHIND ROW 11 MISSING. PHOTOLUMINESCENT FLOOR LIGHTING STRIP INSTALLED IN ROW 11(FWD) REF AMM 33-51-01.
2009
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 10,273 hrs · 7,209 cycles
EMERGENCY LIGHTS STAY ON IN ARM MODE. CYCLED AC PWR, OPS CHECKED, EMERGENCY LIGHTS NO MESSAGE ON EICAS. ACFT RETURNED TO SERVICE IAW AMM 33-24-07.
Part: GLOWSTRIP — MISSING (CABIN) · airframe 9,387 hrs · 6,519 cycles
FLOOR EMERGENCY PHOTO ILLUMINESCENT STRIP MISSING AT EMERGENCY EXIT ON LT SIDE. INSPECTED FLOOR AND FOUND STRIP UPSIDE DOWN, REINSTALLED EMERGENCY STRIP IAW MM 33-51-01.