N9617R
Registered owner: JETRAN LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Airlines | Operator | 2008-12-26 – 2008-12-26 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2008-12-26 – 2008-12-26 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT NOT GROUNDED: PILOT REPORTS UNCOMMANDED AUTO THROTTLE DISCONNECT MULTIPLE TIMES IN CRUISE. ***SUPPLEMENTAL ACTION SECT 4: AIRCRAFT RETIRED ROW. ITEM TRANSFERED TO WO 001992, CARD 01-0012.***(CLOSED)
AIRCRAFT WAS GROUNDED: PILOT REPORTS NR 1 DFGC FAILED ON TAKEOFF ABOVE 80 KTS. NR 1 FD WENT BLANK, AT DISCONNECTED, NR 1 FMA WENT BLANK, DFGC CONTROL PANEL WENT BLANK AND ART FIRED, AFTER T.O SWITCHED TO DFGC, AP NR 2. MAINTENANCE REPORTS DFGC-1 SHOWS DUAL COMP FAILURE-DFGC 0047-DFGC AND RAM FAILURE-DFGC IAW AMM 22-01-05-101-5, ALL FUNCTIONS FROM ASSOC DFGC LOST. REMOVED AND REPLACED DFGC-1. OPS TEST GOOD.
THE CEILING EMERGENCY LIGHT WAS INOPORATIVE AT SEAT 16DEF. REMOVED AND REPLACED THE BATTERY PACK AT BS 671 IAW AMM 33-53-00. OPS CHECKED GOOD.
THE PORTABLE EMERGENCY LIGHT DOES NOT COME ON. REPLACED THE PORTABLE EMERGENCY LIGHT IAW AMM 33-50-00. OPS CHECKED GOOD.
THE EMERGENCY LIGHTS ARE OUT AT THE CENTER CEILING PANEL, ROW 20. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-53-00. OPS CHECKED GOOD.
NOSE GEAR FAILED TO DEPLOY WHEN GEAR HANDLE SELECTED DOWN. RED GEAR UNSAFE LIGHT ILLUMUMINATED FOR THE NOSE GEAR. MAIN GEAR DEPLOYED NORMALLY, USED ALTERNATE GEAR EXTENSION PROCEDURE TO OBTAIN NOSE GEAR DOWN AND LOCKED INDICATIONS, INCLUDING A NOSE LANDING GEAR INDICATION. THE AIRCRAFT WAS GROUNDED. REPLACED THE NOSE LANDING GEAR BUNGEE CYLINDER IAW AMM 32-32-07-201. LEAK AND OPS CHECKED GOOD.
PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED THE PORTABLE EMERGENCY LIGHT IAW AMM 33-53-00.
RIGHT CUSP WEB AFT OF BS 465 HAD A CRACK OUTBOARD SIDE OF LIGHTNING HOLE. REPAIRED THE CUSP WEB IAW 53-20-00-16.
LEFT SIDE WINDOW RING PAN CRACKED LOWER AFT CORNER BETWEEN BS 904 TO 905. INSTALLED A REPAIR DOUBLER IAW 53-10-00-25.
LEFT SIDE WINDOW RING PAN CRACKED TOP FORWARD CORNER BETWEEN BS 807 TO 809. INSTALLED A REPAIR DOUBLER IAW 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT UPPER CORNER BETWEEN STA 1079 TO STA 1098. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
MID CARGO BAY LOWER DOOR FRAME AT BS 664 - 673 CORRODED BELOW DOUBLER. THE CORROSION WAS REMOVED AND INSTALLED A REPAIRED DOUBLER IAW 53-10-00-3.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT LOWER CORNER BETWEEN STA 1003 TO STA 1022. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT UPPER CORNER BETWEEN STA 1022 TO STA 1041. INSTALLED DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT UPPER CORNER BETWEEN STA 1060 TO STA 1079. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT LOWER CORNER BETWEEN STA 1079 TO STA 1098. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED TOP AFT CORNER BETWEEN STA 1022 TO STA 1023. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT AFT LOWER CORNER BETWEEN STA 1041 TO STA 1060. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND SIDE CABIN WINDOW RINGPAN CRACKED AT FORWARD LOWER CORNER BETWEEN STA 984 TO STA 1003. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. CRACKED WINDOW RING PAN AT STA 1060 TO STA 1061. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
AIRCRAFT IN BASE MAINTENANCE. CRACK AT AFT RIGHT HAND NOSE GEAR DOOR, AFT HINGE CUTOUT. INSTALLED DOUBLER AND EDGE SEALED PER SRM 53-05-00-001, FIGURE 158 AND DRAWING SGO9530030.
THE AIRCRAFT IS IN BASE MAINTENANCE. CUSP SHEET AT STATIONS 1193-1212 ON RIGHT HAND SIDE HAS CORROSION ALL THE WAY THROUGH CUSP SHEET. REPAIRED CUSP SHEET PER 53-20-00-16.
AIRCRAFT IN BASE MAINTENANCE. SIDE CABIN WINDOW RINGPAN CRACKED BETWEEN STA 984 TO STA 985. INSTALLED REPAIR DOUBLER PER 53-10-00-25.
LEFT SIDE WINDOW RING PAN CRACKED AT BS 1022 TOP AFT CORNER. INSTALLED DOUBLER IAW 53-10-00-25.
LEFT WINDOW RING PAN CRACKED AT BS 1079 TOP AFT CORNER. INSTALLED A DOUBLER IAW 53-10-00-25.
LEFT SIDE WINDOW RING PAN CRACKED AT BS 1041 TOP AFT CORNER. INSTALLED DOUBLER IAW 53-10-00-25.
AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON CUSP LOCATED AT STA 560, RIGHT SIDE. REPLACED CUSP PER 53-20--00-16.
LEFT SIDE WINDOW RING PAN CRACKED AT BS 1231. INSTALLED A REPAIR DOUBLER IAW 53-10-00-25.
CORROSION ON THE CUSP WEB BETWEEN BS 845 AND 905 RIGHT SIDE UNDER SEAT TRACK NR 6. REPLACED THE CUSP WEB IAW DRAWING FDK3203, 51-00-05-1, AND SRM 51-10-03.
AIRCRAFT WAS GROUNDED: SLIDE ON L2 DOOR OUT OF COVER. MAINTENANCE REPLACED AFT GALLEY SERVICE DOOR SLIDE PER AMM 25-62-00A AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
FORWARD MEGAPHONE VOLUME TOO LOW. REMOVED AND REPLACED THE MEGAPHONE IAW MM 23-34-00. OPS CHECKED NORMAL.
FORWARD MEGAPHONE VOLUME TOO LOW. REPLACED FORWARD MEGAPHONE IAW MM 23-34-00. OPS CHECKED NORMAL.
R1 WINDOW DELAMINATED, OUT OF LIMITS. REPLACED THE FIRST OFFICER`S SIDE WINDOW IAW MM 52-10-02. AIRCRAFT WAS GROUNDED.
L1 WINDOW DELAMINATED OUT OF LIMITS. REPLACED CAPTAINS SIDE WINDOW IAW MM 56-10-02. AIRCRAFT WAS GROUNDED.
AIRCRAFT WAS GROUNDED. EMERGENCY PATH LIGHT BATTERY BS-103 REQUIRES REPLACEMENT. REPLACED EMERGENCY PATH LIGHT BATTERY PACK PER WDM 33-51-12.
AIRCRAFT WAS GROUNDED. EMERGENCY PATH LIGHT BATTERY AT POSITION BS-105 REQUIRES REPLACEMENT. REPLACED EMERGENCY PATH LIGHT BATTERY AT BS-105 PER WDM 33-51-12.
FLASHLIGHT LED NOT FLASHING AFT FLIGHT ATTENDANT SEAT. REPLACED FLASHLITE BATTERY. OPERATIONS CHECK NORMAL PER MM 25-60-00
EMERGENCY EXIT LIGHTS IN THE TAIL COMPARTMENT ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-28 IAW AMM 33-53-00. OPS CHECKED GOOD.
SINGLE TAIL CONE EMERGENCY SLIDE LIGHT IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-27 IAW AMM 33-53-00. OPS CHECKED GOOD.
EMERGENCY EXIT CEILING LIGHTS FROM ROWS 12 TO 16 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK B5-102 IAW AMM 33-53-00. OPS CHECKED GOOD.
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE FORWARD ENTRY DOES NOT SHOW A CHARGE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.
EMERGENCY LIGHTS INOP AT MID GALLEY OVERHEAD. R&R BATTERY PACK B5-107. LIGHTS OP CK OK. THE AIRCRAFT WAS NOT GROUNDED.
EMERGENCY LIGHTS INOP AT MID GALLEY OVERHEAD . R&R BATT PACK B5-107 IAW MM 33-53-00. EMERGENCY LT OP OK. THE AIRCRAFT WAS NOT GROUNDED.
ESCAPE PATH MARKERS FAILED DUAL FEED CHECK, IAW MCM CARD 5403. REPLACED CONNECTOR AT SIDEWALL SYSTEM OP-CHECKS OK, IAW MCM 5403. THE AIRCRAFT WAS NOT GROUNDED.
NO GEAR LIGHTS WITH GEAR HANDLE DOWN. FOUND LANDING GEAR WARNING BREAKER OUT. NOSE GEAR LIGHT REMAINED OUT AFTER RESETTING BREAKER AND SPARKS FROM NOSE GEAR INDICATOR WHEN RESETTING. MAINTENANCE INSPECTED LIGHT ANNUNCIATOR FOR GEAR POSITION INDICATION AND FOUND CAUSE OF DISCREPANCY. REMOVED AND REPLACED LANDING GEAR ANNUNCIATOR, OPERATIONALLY CHECKS NORMAL IAW AMM 32-60-03 AND WDM 32-61-00. THE AIRCRAFT WAS GROUNDED.
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. SDF-DFW FLIGHT RETURNED TO SDF ACCOUT OF HORIZONTAL STABILIZER PRIMARY TRIM INOPERATIVE. LANDING UNEVENTFUL. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR IAW AMM 27-40-01. OPERATIONAL CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE. SKIN CRACK AT FUSELAGE STATION 1418 AND L2L. REPAIRED IAW SRM 53-04-00.
AIRCRAFT GROUNDED. FIRST CLASS EMERGENCY LIGHTS CAME ON AT SHUTDOWN AND ARE NOW FULLY DISCHARGED. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT LENS SHROUD AT SEAT 31D IS BROKEN. REMOVED AND REPLACED LENS SHROUD IAW AMM 33-60-98. OPERATIONAL CHECK NORMAL IAW AMM 33-60-98-501.
AIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY PATH LIGHTS DIM WHEN TESTED WITH BATTERY PACK AB5-4. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-60-98. SYSTEM CHECKS NORMAL.
AIRCRAFT WAS NOT GROUNDED. OVERHEAD EMERGENCY LIGHTS IN 1ST CLASS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY FOR 1ST CLASS OVERHEAD LIGHTS IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL.
AFTER GEAR EXTENSION, NO NOSE GEAR GREEN DOWN AND LOCKED LIGHT. FOLLOWED QRH, DID FLY BY--TOWER VERIFIED NOSE GEAR DOWN. LANDING NORMALLY. RELAMPED BOTH NLG GREEN DOWN AND LOCK LAMPS. OPS CK"D NORMAL. REMOVED GEAR PINS THAT WERE INSTALLED TO TAXI TO THE GATE. THE AIRCRAFT WAS NOT GROUNDED.
AIRCRAFT WAS GROUNDED. AIR INTERRUPT, DURING CRUISE NR 1 ENGINE GENERATOR OFF LIGHT CAME ON, VOLTS NORMAL. BETWEEN 1801 AND RED LINE DISCONNECTED IAW QRH. MAINTENANCE R & R NR 1 ENGINE GENERATOR IAW AMM 24-20-01 AND NR 1 ENGINE CONSTANT SPEED DRIVE OIL COOLER IAW AMM 24-10-01. LEAK AND OPS CHECKS NORMAL. ALSO AALA20160622008.
AIRCRAFT WAS GROUNDED. AIR INTERRUPT DURING CRUISE, NR 1 ENGINE GENERATOR OFF LIGHT CAME ON, VOLTS NORMAL. BETWEEN 1801 AND RED LINE DISCONNECTED IAW QRH. MAINTENANCE R & R NR 1 ENGINE GENERATOR IAW AMM 24-20-01 AND NR 1 ENGINE CONSTANT SPEED DRIVE OIL COOLER IAW AMM 24-10-01. LEAK AND OPS CHECKS NORMAL, ALSO AALA20160624007.
AIRCRAFT WAS NOT GNDED. EMER PATH LIGHT AT SEAT 6DF IS INOPERATIVE. FOUND LOOSE CONNECTOR. SECURED CONNECTOR & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-60-98. SYSTEM CHECKED NORMAL.
AIRCRAFT NOT GNDED. EMERGENCY LIGHT AT TAIL CONE COMPARTMENT & CAT WALK INOPERATIVE. FOUNDED LOOSE CONNECTOR AT BATTERY PACK B5-28. SECURED CONNECTOR & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-53-00. SYS CHECKED NORMAL.
AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB NLG WOULD NOT RETRACT. FOUND NOSE STRUT LEAKING & BOTTOMED OUT CAUSING NO RETRACTION OF NOSE GEAR. R & R NOSE GEAR PISTON IAW AMM 32-21-02. ACCOMPLISHED NLG SWING. OK FOR SERVICE.
RETURNED, RT ENG FIRE HANDLE ILLUMINATED ALONG WITH AURAL WARNING ON CLIMB OUT. AN EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. FOUND ANTI-ICE TUBE ON TOP OF RT ENG BLOWN. REPLACED RT ENG ANTI-ICE DUCT IAW AMM 75-10-02.
FLIGHT DIVERTED, RT ENG START VLV LIGHT ILLUMINATED IN FLIGHT. CREW SHUTDOWN RT ENG. SINGLE ENG TIME WAS 15 MINUTES. AN EMER LANDING WAS DECLARED. LANDING UNEVENTFUL. THE ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED MCM PROCEDURES ON MEL 80-01, DEFERRED RT ENG START VLV ON MEL PLACARD. REPLACED RT ENG STARTER CONTROL VLV IAW AMM 80-10-02 & CLEARED MEL PLACARD.
AFTER TAKEOFF, CLIMBING THROUGH 15,000 FT, RECEIVED RT ENG OIL FILTER CLOG INDICATION. ALL ENG PARAMETERS WERE NORMAL. IAW QRH, ENG WAS RETARDED TO IDLE FOR LANDING. EMER DECLARED, RETURNED & LANDED UNEVENTFULLY. ACFT WAS REMOVED FROM SERVICE. RT ENG STRAINER CLOGGED LIGHT CHECKED & APPROVED FOR DEFERRAL IAW MEL 79-3. INSTALLED PLACARD & ENTERED IN MIC SHEET, OPEN. REPLACED NR 2 ENG OIL STRAINER CLOG SWITCH.
LEFT NOSE, AFT GEAR DOOR AFT SKIN CUT OUT CRACKED. INSTALLED REPAIR DOUBLER IAW SRM 53-05-00-001 FIGURE 158.
CORROSION ON FORWARD CARGO DOOR PAN LOWER SECTION AT LONGERON 25R BETWEEN BS 370 & 427. REPAIRED PAN DAMAGE & INSTALLED FILLER WITH STRAP EA 253265.
DURING CLIMB, AFT GALLEY DOOR LIGHT ILLUMINATED. AFTER RETURNING & LANDING, AFT GALLEY DOOR LIGHT EXTINGUISHED. EMERGENCY DECLARED, RETURNED TO DEPARTURE AND LANDING WAS UNEVENTFUL. UPON GATE ARRIVAL, FOUND PRESSURIZATION IN MANUAL MODE. ACCOMPLISHED AUTO GROUND PRESSURIZATION TEST IAW AMM 21.32.00. AFT GALLEY DOOR PROXIMITY SENSOR CHECKED GOOD. SYS CHECKED NORMAL.
FORWARD OVERWING EMER EXIT EMER LIGHTS WON`T TEST. R & R FWD OVERWING EMER LIGHT BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.
TAIL COMPARTMENT EMER LIGHTS WON`T TEST. R & R TAIL COMPARTMENT EMER LIGHT BATTERY PACK B5-28 IAW AMM 33-53-00. SYS CHECKED NORMAL.
OVERHEAD EMER LIGHTS AT AFT FLIGHT ATTENDANT SEAT WON`T TEST. R & R EMER LIGHT BATTERY PACK B5-27 FOR AFT FLIGHT ATTENDANT SEAT AREA IAW AMM 33-53-00. SYS CHECKED NORMAL.
FIRST CLASS OVERHEAD EMER LIGHTS WON`T TEST. R & R FIRST CLASS EMER LIGHT BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.
LEFT AFT TIE DOWN TRACK IN AFT CARGO CORRODED. INSTALLED NEW TRACK SECTION IAW AARD 51-00-05-1.
LEFT FWD TIE DOWN TRACK IN AFT CARGO CORRODED. INSTALLED NEW TRACK IAW AARD 51-00-05-1.
ANGLE CRACKED AT INTERCOSTAL BELOW NR 5 SEAT TRACK AT STATION 826. INSTALLED REPAIR STACK DOUBLER IAW EA MD80-57-034310.
SEAT TRACK NR 4 FROM STATIONS 224 TO 226 CORRODED. REPLACED NR 4 SEAT TRACK FROM STATION 200 TO STATION 304 IAW SRM 53-05-00 FIGURE 4F.
NR 4 SEAT TRACK FROM STATIONS 1276 TO 1279 CORRODED. INSTALLED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10.
NR 4 SEAT TRACK CORRODED FROM STATIONS 838 TO 840. PERFORMED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10.
CRACK & CORROSION ON CUSP SHEET FROM STATIONS 218 TO 237 RT. REPLACED CUSP SHEET IAW AARD 51-00-05-1 & AARD 53-20-00-16.
ELONGATED ATTACHMENT HOLE IN RT CUSP AT NR 5 SEAT TRACK & STATION 242. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.
CORROSION ON SUBFLOOR AT STATION 217 RT. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.
CABIN FLOOR BEAM INTERCOSTAL CRACKED FROM STATIONS 1287 TO 1309. INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.
AFT CARGO Z CHANNEL CORRODED AT STATION 1131 RT SIDE. INSTALLED NEW CHANNEL IAW SRM 51-30-01.
CORROSION AFT CARGO DOOR BEAM. INSTALLED DOUBLER IAW AARD 53-10-00-3.
CORROSION UNDER G1 GALLEY DRAIN PAN. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.
FUSELAGE SHEAR TIE CRACKED AT AFT SIDE OF STATION 1437 FRAME AT LONGERON 2 LT. REMOVED & INSTALLED NEW SERVICEABLE SHEAR TIE IAW AARD 51-00-05-1.
CORROSION ON INTERNAL DOUBLER AT LOWER FWD SIDE OF AFT LAVATORY SERVICE DOOR CUT OUT. ROUTED OUT CORROSION & INSTALLED DOUBLER & FILLER IAW EA.
WEAR AT BS 1380 FRAME FWD SIDE AT TEMPERATURE CONTROL VLV. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-28.
SUB FLOOR CRACKED AT BS 216 UNDER SEAT TRACK NR 4. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.
RIGHT HAND CUSP WEB BS 1184 - 1190 CORRODED. REMOVED CORROSION & INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.
LEFT CUSP WEB CORRODED FROM BS 508 - 509. REMOVED CORROSION & INSTALLED DOUBLER IAW RD 53-20-00-16.
SEAT TRACK NR 6 FROM STATIONS 997 TO 999 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
CORROSION ON CUSP FROM STATIONS 390 TO 391, OTBD UNDER NR 6 SEAT TRACK. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.
CORROSION ON CUSP FROM STATIONS 388 TO 389. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.
SEAT TRACK NR 6 FROM STATIONS 629 TO 634 CORRODED. INSTALLED SEAT TRACK PLUG IAW SRM 53-05-00-001.
SEAT TRACK NR 6 FROM STATIONS 662 TO 673 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
SEAT TRACK NR 6 FROM STATIONS 693 TO 700 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
SEAT TRACK NR 6 FROM STATIONS 726 TO 729 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
SEAT TRACK NR 6 FROM STATIONS 757 TO 759 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
SEAT TRACK NR 6 FROM STATIONS 1027 TO 1031 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
SEAT TRACK NR 6 FROM STATIONS 1058 TO 1062 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
CORROSION ON NR 5 SEAT TRACK FROM STATIONS 233 TO 237. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-05-00 FIGURE 4F.
CORROSION ON NR 6 SEAT TRACK FROM STATIONS 263 TO 407 CORRODED. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-05-00 FIGURE 4F.
SEAT TRACK NR 6 FROM STATIONS 1277 TO 1280 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
SEAT TRACK NR 6 FROM STATIONS 934 TO 938 CORRODED. INSTALLED NEW SEAT TRACK PLUG IAW SRM 53-05-00-001.
FWD SECTION OF CABIN SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED MODULE AB5-2. OPERATIONS CHECKED NORMAL.
TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAILCONE EMERGENCY LIGHTS, OPERATIONS CHECKED NORMAL.
ORD - CREW REPORTED UPON GEAR EXTENSION, NO NOSE GEAR DOWN INDICATION AND NO NOSE LANDING GEAR PIN EXTENSION INDICATION. FLIGHT ACCOMPLISHED GO AROUND AND CONFIRMED GEAR DOWN. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE GEAR BUNGEE CYLINDER. SYSTEM GROUND CHECK NORMAL OPERATION.
ACCIDENTAL IMPACT TO STATION 1416.5 BETWEEN LONGERONS 6 AND 7 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER SRM SG09530001 VIEW E.
DFW - CREW REPORTED FUMES IN CABIN DURING FLIGHT. ACCOMPLISHED QHR. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND BLOWN ANTI-ICE DUCT ON NUMBER 1 ENGINE. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.
BIL - INFLIGHT DFW-YYC. IN CRUISE, CREW OXYGEN BOTTLE DEPLETED. FLIGHT LANDED BIL WITHOUT INCIDENT. MAINTENANCE REPLENISHED OXYGEN. SYSTEM GROUND CHECK NORMAL OPERATION.
FOUND EMERGENCY EXIT LIGHT COVER CRACKED. REPLACED COVER FOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.
DFW - CREW REPORTED STRONG ELECTRICAL SMELL ON DESCENT IN THE AFT OF CABIN. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED OVERHEAD LIGHT BALLAST AND LAMP AT 25-26DEF THAT WAS INOPERATIVE. SYSTEM GROUND CHECKED NORMAL OPERATION.
LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED OVERWING EXIT LIGHT BATTERY PACK.
AFT 1418 FRAME CRACKED AT LONGERON 2 RIGHT. INSTALLED DOUBLER AT FRAME 1418 AT LONGERON 2 RIGHT PER ENGINEERING AUTHORIZATION MD80-53-008173 ISSUE DATE 11-19-09.
AFT LAVATORY SERVICE PAN AT FORWARD LOWER CORNER HAS CORROSION. REPLACED LAVATORY PAN UNDER AARD 53-30-00-7.
LEFT WING INBOARD FLAP INBOARD WEDGE INBOARD RIB IS CRACKED OUT AT FORWARD END. REMOVED RIB, INSTALLED NEW MANUFACTURED MODIFIED RIB REF SRM 57-01-00 FIG 3 SHEET 2 AND 51-01-00.
CORROSION ON FRAME 1287, LONGERON 29 RIGHT TO LONG 29 LEFT. INSTALLED FORMER REPAIR SPLICE PER SRM 53-03-00.
CORROSION FOUND ON CUSP. INSTALLED DOUBLER UNDER AARD 53-20-00-16.
MID CARGO CORROSION ON LOWER SIDE OF RIGHT CUSP. INSTALLED NEW CUSP SHEET RIGHT HAND STATION 598-712 PER AARD 53-20-00-16.
CORROSION ON DOOR JAMB FORWARD FITTING. REPLACED FITTING.
TRAP FITTING AT FORWARD UPPER ATTACH ANGLE IN RIGHT HAND WHEEL WELL DAMAGED. REMOVED AND REPLACED TRAP FITTING.
CORROSION ON BOTTOM OF CUSP AT STATION 680. INSTALLED DOUBER PER AARD 53-20-00-16.
LEFT CUSP CORROSION IS BEYOND LIMITS FOR STATION 218 TO 237. INSTALLED NEW CUSP SHEET AND LIGHTNING HOLE DOUBLER PER SRM 51-30-05 AND AARD 53-20-00-16.
NUMBER 1 FLAP VANE AT BOTTOM SIDE HAS DENT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER WITH HOT BOND PER SRM 71-50-02.
AFTER CORROSION REMOVAL ON RIGHT SIDE CUSP AT STATION 886-905, INSUFFICIENT MATERIAL LEFT, OUT OF LIMITS. INSTALLED DOUBLER ON RIGHT CUSP AT STATION 886-905 PER AARD 53-20-00-16.
LEFT CUSP CORROSION IS BEYOND LIMITS AT STATION 541 TO 560, INSTALLED DOUBLER ON LEFT HAND CUSP STATION 541 TO 560 PER AARD 53-20-00-16.
AFT SERVICE DOOR HANDLE PAN HOUSING GOUGED. REMOVED AND INSTALLED NEW HANDLE PAN PER ESO 80175.
FORWARD ENTRY DOOR HAS CRACK AT NUMBER 6 BEAM AT BAYONET BRACKET ATTACH BOLT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO NR 80172.
WINDOW PAN CRACKED AT STATION 807 RIGHT FORWARD UPPER EAR. PERFORMED DOUBLER REPAIR UNDER AARD53-10-00-25.
FORWARD CARGO DOOR STOP PAD BRACKET CRACKED AT TOP FORWARD DOOR EDGE. INSTALLED A NEW STOP PAD BRACKET PER ESO 80174.
E AND E COMPARTMENT CEILING MEMBRANE HAS CORROSION ALONG AFT SIDE OF CABIN FLOOR BEAM AT STA 200, APPROX 10 INCHES INBOARD ON RIGHT HAND CUSP. INSTALLED DOUBLER PER AARD 53-20-00-16.
ESCAPE PATH LIGHTS FROM FIRST CLASS GALLEY TO ROW 19DEF ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT FIRST CLASS LAVATORY PER MM, OPS CHECK OK.
TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK AND CHARGER IN AFT LAV. OPS CHECK NORMAL AFTER BATTERY CHARGED.
FORWARD ENTRY AND FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE DURING TEST. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSEMBLY IN OVERHEAD COMPARTMENT. OPS CHECKS NORMAL.
OVERHEAD CEILING EMERGENCY LIGHT OVER 18D INOPERATIVE DURING LIGHT TEST. RELAMPED LIGHT. OPS CHECKS NORMAL.
ORD EMERGENCY LIGHTS AT SEAT ROWS 19DEF TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 19DEF TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
MCI INFLIGHT T1964/08MAY - CREW REPORTED ACCESSORY COMPARTMENT OVERHEAT INDICATION. RETURNED TO MCI AND LANDED WITHOUT INCIDENT. FOUND RIGHT TEMPERATURE CONTROL VALVE DUCT BOOT LEAKING. REPLACED BOOT AND CLAMPS FOR RIGHT TEMPERATURE CONTROL VALVE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY EXIT MARKER AT AFT DOOR NEAR FLOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MARKER AT AFT DOOR NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY EXIT MARKER AT AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT MARKER AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY EXIT MARKER AT TAIL COMPARTMENT LEFT SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MARKER AT TAIL COMPARTMENT LEFT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT 13D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT 16C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY EXIT MARKER AT LEFT TAIL COMPARTMENT SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MARKER AT LEFT TAIL COMPARTMENT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY EXIT MARKER AT FORWARD GALLEY WALL AT FLOOR LEVEL INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT MARKER AT FORWARD GALLEY WALL AT FLOOR LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT ROW 32 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 32. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT ROW 31 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT ROW 30 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT ROW 8 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION.
PHX INFLIGHT T1782/07JAN SAN - DFW AT FLIGHT LEVEL 310, LEFT GENERATOR TRIPPED ON AND OFF SEVERAL TIMES. CONSTANT SPEED DRIVE OIL TEMPERATURE OVER RED LINE. UNABLE TO START APU. TURNED LEFT GENERATOR SWITCH OFF. CONSTANT SPEED DRIVE OIL TEMPERATURE COOLED BELOW RED LINE. LANDED PHX WITHOUT INCIDENT. REPLACED LEFT CONSTANT SPEED DRIVE AND GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 3, 5, 7, AND 11. RESEATED THE LAMPS AT ALL 4 POSITIONS. CHECK-C 9-11-02 STL.
THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 20 TO 23. RESEATED THE BATTERIES IN THE BATTERY PACK. CHECK-C 9-11-02 STL.
THE LEFT SIDE FORWARD CABIN DOOR ESCAPE SLIDE HAD LOW BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHECK-C 10-11-01 MCI. --CLOSED--
DURING CHECK-C MAINT ON THE AFT FUSELAGE EXTERIOR, LT SIDE 3 INCHES FWD OF VERTICAL FIN REAR SPAR, A CRACK WAS FOUND BETWEEN FASTENERS IN THE ATTACH ANGLE. CONFIRMED BY EDDY CURRENT. ACCOMP HIGH FREQ EDDY CURRENT AND FOUND CRACK CONTAINMENT PER NDT MANUAL 51-00-03, PART 6. REPAIRED PER SRM 53-05, PAGE 49.
DURING CHECK-C MAINT ON THE LT WING L/E, A CRACK WAS FOUND AT DOUBLER AT LOWER L/E OPENING BETWEEN NUMBER 5 AND 6 L/E SLAT TRACK. ACCOMP EDDY CURRENT INSPECTION PER NDT 51-00-03 AND FOUND CRACK CONTAINED. FABRICATED DOUBLER REPAIR PER SRM 57-01, PAGE 9, AND SRM 51-10-3, PAGE 16. INSTALLED PER SRM 51-30-1 AND 51-30-5.
DURING CHECK-C MAINT ON THE LT MAIN GEAR WHEEL WELL, APPROX STA 946, LBL 7, THE FWD INBD CORNER OF THE GEAR WELL WAS CRACKED AND BUSTED. ACCOMP EDDY CURRENT INSP PER NDT 51-00-03 AND FOUND CRACK CONTAINED. REPAIRED PER SRM 53-01, PAGE 10, TWO REPAIR ANGLES.
IN FLIGHT THE RT ENGINE FIRE WARNING GIVE VISUAL AND AURAL SIGNAL. REDUCED THROTTLE TO IDLE, NO HELP. SHUT DOWN ENGINE AND FIRED BOTH BOTTLES, STILL NO HELP. LANDED AT SCHEDULED STATION, SJU. FOUND THE CENTRAL AURAL WARNING SYSTEM (CAWS) AT FAULT FOR ERRONEOUS INDICATION, AND REPLACED SAME. ALSO REPLACED BOTH ENGINE FIRE WARNING LOOPS PRECAUTIONARY, AND THE UNITS NECESSARY TO RESTORE THE FIRE EXTINGUISHING SYSTEM. CHECK-C 10-8-00 JFK.
THE EGRESS LIGHTS WERE INOPERATIVE AT ROWS 3 TO 5. RESEATED THE BULBS AND WORKED NORMAL. CHECK-C 10-8-00 JFK.
CREW REPORTED SMOKE IN CABIN AT LIFT OFF. FLIGHT RETURNED TO STL. FOUND OIL IN APU INLET. OTHER CHECKS NEGATIVE. SUSPECT APU OIL WAS OVERSERVICED. CLEANED UP OIL AND ACCOMPLISHED PACK BURN OUT. CHECK-C 10-8-00 JFK.
THE EGRESS LIGHTS WERE INOPERATIVE AT THE FWD GALLEY AND AT ROW 11 TO 15. REPLACED LIGHT MODULE (P/N 0105606-002) AT FWD GALLEY, AND MODULES 0105606-003 AND 0105606-004 AT ROWS 11 TO 15. CHECK-C 9-31-99 STL.
THE OVERHEAD LIGHT CABIN ROW 27 RT SIDE WAS ARCING AND HAD AN ODOR. CREW REMOVED THE BULB. MAINTENANCE REMOVED THE CONNECTOR FROM THE LIGHT BALLAST AND DEFERRED CORRECTIONS PER MEL. NO CHECK-C. *S/D* FOUND LAMPHOLDERS HAD BURNED CONTACTS CAUSED BY LAMP NOT PROPERLY SEATED IN LAMPHOLDERS. REPLACED THE LAMPHOLDERS.
THE FWD LEFT SIDE CABIN DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE ESCAPE SLIDE.