N804NN
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Airlines | Operator | 2011-09-29 – 2011-09-29 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2011-09-29 – 2011-09-29 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT WAS NOT GROUNDED: LIGHT OVER EXIT ROW AT 14F STROBING. PASSENGER/FLIGHT ATTENDANT CONCERNED COULD CAUSE A SEIZURE. MAINTENANCE PERFORMED RESET OF LIGHTS IN CABIN IAW AMM 33-20-00.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORT THAT THE AFT RIGHT LAVATORY DOOR STICKS AND IS DIFFICULT TO OPEN AND CLOSE. ADJUSTED DOOR THRESHOLD TO ALLOW PROPER DOOR CLEARANCE. PER AMM 25-40-08. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: EGT OVER TEMP ON THE NUMBER 2 ENGINE. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT DFW. ACCOMPLISHED AMM 71-00-00-800-804-F00 AND CONTACTED ENGINE DESK FOUND NUMBER 2 ENGINE EXCEEDANCE IN AREA "B" NO EEC FAULTS ENGINE IS LOW MARGIN ENGINE. NUMBER 2 ENGINE IS OKAY FOR CONTINUED SERVICE. WITHIN ENGINE LIMITS.
AIRCRAFT WAS NOT GROUNDED: AFTER RIGHT LAVATORY DOOR WON'T OPEN. TIGHTENED LOOSE SCREW ON AFT RIGHT HAND LAVATORY DOOR LATCH ASSEMBLY. OPERTIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAVATORY DOOR JAMMED SHUT AND UNABLE TO OPEN. UNJAMED DOOR. PER AMM 25-40-00.
AIRCRAFT WAS GROUNDED: FIRST CLASS GALLEY NUMBER 1 OVEN, HAS A BURNING SMELL DURING OPERATION. (OPEN).
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: SHORTLY AFTER ROTATION WE NOTICED AN ODOR. IMMEDIATELY AFTER THE ODOR WE RECEIVED A LAV SMOKE INDICATION, AND FLIGHT ATTADNENT CALLED AND REPORTED FOUL ODOR AND LAVATORY SMOKE DETECTOR GOING OFF IN FORWARD LAVATORY AS WELL, ODOR IS LIKE A BURNT FUEL AND EXHAUST SMELL. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT ORD. ACCOMPLISHED WORKCARD 08L00021001 FOR SMOKE ODOR FUMES, PREFORMED PACK BURN TO REMOVE SMOKE.
AIRCRAFT WAS GROUNDED: FIRST CLASS GALLEY NUMBER 1 OVEN, HAS A BURNING SMELL DURING OPERATION. **SUPPLEMENTAL REPORT FOR (AALA202502141457): OPERTIONAL CHECK AND CLEAN THE NUMBER 1 OVEN. PER AMM 25-32-02 **(CLOSED).
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AFTER INCREASING THRUST LEVERS TO 70% SMOKE AND HAZE BEGAN TO FILL THE COCKPIT; AIRCRAFT GROUND INTERRUPTED BACK TO GATE SAFELY AT ORD. PERFMORD J/C 08L00021001, COULD NOT REPLICATE SMELL, DE-ICE FLUID WAS HEAVILY PREVELANT AROUND APU AMD ENGINE INLETS. NO DEFECTS NOTED. NO FAULT FOUND.
AIRCRAFT WAS NOT GROUNDED: LEFT AFTER LAVATORY DOOR DIFFICULT TO OPEN IN FLIGHT. LUBED DOOR LATCH ASSEMBLY ON AFT LEFT LAVATOPRY AND OPERTIONAL CHECK GOOD. PER CMM 25-40-64.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON CLIMB OUT AT ROUGHLY 5000 FEET WE HAD THE MC AND EQUIP DOOR ILLUMINATE. IN ADDITION THE AIRCRAFT WAS NOT PRESSURIZING AT 8000 FEET. DESCENDED TO 4000 AND RAN QRH PROCEDURES; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT RDU. REMOVE AND REPLACED CABIN PRESSURE CONTROLLER. OPERTIONAL CHECK GOOD. PRESSURIZATION SYSTEM GROUND TEST ACCOMPLISHED. SYSTEM PASSED. PER AMM 21-31-01.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER AT STA 663.75, LBL 31.83. REPAIRED CRACK PER SRM 57-10-10-2R-2 AND AARD 57-10-10-9.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ABOVE OVERHEAD STOWAGE BIN AT SEAT 16FED IS INOPERATIVE. DURING EMERGENCY LIGHT TEST INSPECTION CHECK SEAT ROW 16FED FOUND CONNECTOR LOOSE. RECONNECT AND PERFORMED TEST, TEST GOOD. PER AMM 33-51-00.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ABOVE OVERHEAD STOWAGE BIN AT SEAT 16FED IS INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
AIRCRAFT WAS NOT GROUNDED: L1 DOOR GIRT BAR MISSING RED PLASTIC COVERING ON OUTER EDGE. INSTALLED HEAT SHRINK MISSING AT NUMBER 1L DOOR. PER AMM 25-66-00.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLIGHT DIRECTOR DISAPPEARED ON APPROACH AGAIN. AIRCRAFT DIVERTED AND LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. FOUND FAULT MSG 22-11051. ACCOMPLISHED FIM 22-11-00. REMOVED AND REPLACED NUMBER 1 FORWARD ANTENNA (AALA202401090977), NUMBER 1 AFT ANTENNA (AALA202401098436), NUMBER 2 FORWARD ANTENNA (AALA202401096029), AND NUMBER 2 AFT RADAR ANTENNAS (AALA202401090549). ALL BITE TEST PASSED INCLUDING DFCS BITE TEST.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLIGHT DIRECTOR DISAPPEARED ON APPROACH AGAIN. AIRCRAFT DIVERTED AND LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. FOUND FAULT MSG 22-11051. ACCOMPLISHED FIM 22-11-00. REMOVED AND REPLACED NUMBER 1 FORWARD ANTENNA (AALA202401090977), NUMBER 1 AFT ANTENNA (AALA202401098436), NUMBER 2 FORWARD ANTENNA (AALA202401096029), AND NUMBER 2 AFT RADAR ANTENNAS (AALA202401090549). ALL BITE TEST PASSED INCLUDING DFCS BITE TEST.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLIGHT DIRECTOR DISAPPEARED ON APPROACH AGAIN. AIRCRAFT DIVERTED AND LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. FOUND FAULT MSG 22-11051. ACCOMPLISHED FIM 22-11-00. REMOVED AND REPLACED NUMBER 1 FORWARD ANTENNA (AALA202401090977), NUMBER 1 AFT ANTENNA (AALA202401098436), NUMBER 2 FORWARD ANTENNA (AALA202401096029), AND NUMBER 2 AFT RADAR ANTENNAS (AALA202401090549). ALL BITE TEST PASSED INCLUDING DFCS BITE TEST.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: FLIGHT DIRECTOR DISAPPEARED ON APPROACH AGAIN. AIRCRAFT DIVERTED AND LANDED SAFELY AT IAD WITHOUT FURTHER INCIDENT. FOUND FAULT MSG 22-11051. ACCOMPLISHED FIM 22-11-00. REMOVED AND REPLACED NUMBER 1 FORWARD ANTENNA (AALA202401090977), NUMBER 1 AFT ANTENNA (AALA202401098436), NUMBER 2 FORWARD ANTENNA (AALA202401096029), AND NUMBER 2 AFT RADAR ANTENNAS (AALA202401090549). ALL BITE TEST PASSED INCLUDING DFCS BITE TEST.
AIRCRAFT WAS NOT GROUNDED: LAVATORY D DOOR OFF TRACK, DIFFICULT TO OPEN. ADJUSTED LAVATORY DOOR AS REQUIRED. FUNCTIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED: FLIGHT DECK L1 WINDSHIELD ARCED AND THEN THE OUTER PANE CRACKED. MAINTENANCE REPLACED THE WINDSHIELD PER TASK CARD 08L21056007.
AIRCRAFT WAS GROUNDED: R1 WINDSHIELD CRACKED IN FLIGHT. REPLACED R1 WINDSHIELD PER JOB CARD 08L21056004.
AIRCRAFT WAS GROUNDED: REPLACED RIGHT FORWARD OVERWING EXIT LIGHT ASSEMBLY PER AMM 33-21-00. DID NOT FIX, FURTHER TROUBLE SHOOTING REQUIRED. LIGHT ASSEMBLY BAD FROM STOCK REMOVED AND REPLACED RIGHT FORWARD OVERWING EXIT LIGHT ASSEMBLY PER AMM 33-21-01.
AIRCRAFT WAS NOT GROUNDED. THE EVACUATION SLIDE FOR THE R1 SERVICE DOOR IS COMING OUT OF ITS HOUSING. RESECURED R1 DOOR GIRT BAR IAW AMM 25-66-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK OF THE R1 DOOR ESCAPE SYSTEM IAW AMM 25-66-00.
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT LAVATORY DOOR HANDLE IS LOOSE. **SUPPLEMENTAL REPORT FOR AALA202204117764: REPLACED DOOR LATCH ASSEMBLY PER AMM 25-40-15. OPERATIONAL CHECK GOOD.** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT LAVATORY DOOR HANDLE IS LOOSE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
AIRCRAFT WAS GROUNDED: REJECTED TAKEOFF AT APPROXIMATELY 60 KNOTS DUE TO TAKEOFF CONFIGURATION LIGHTS ILLUMINATED. RETURNED TO GATE. REPLACED ANITSKID / AUTO BRAKE CONTROL UNIT PER AMM 32-42-00.
AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR HANDLE FELL OFF. REINSTALLED DOOR HANDLE PER AMM 25-40-15.
AIRCRAFT WAS NOT GROUNDED. FORWARD LAVATORY DOOR LATCH LOOSE. SECURED FORWARD LAVATORY DOOR LATCH.
AIRCRAFT WAS NOT GROUNDED: HANDLE ON AFT LAVATORY DOOR STARBOARD SIDE CAME OFF. INSTALLED DOOR HANDLE PER AMM 52-54-00.
AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY SERVICE DOOR GIRT BAR IS LOOSE IN THE CLIPS IN THE DISARMED POSITION. RE-SECURED FORWARD GALLEY SERVICE DOOR GIRT BAR CLIPS, PER AMM 25-66-00.
AIRCRAFT IN BASE MAINTENANCE: HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70. NEW RIB INSTALLED PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER 3RD STIFFENER FROM THE FRONT IS CRACKED ON RIB AT STA 129.50. INSTALLED NEW RIB PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: BAFFLE LOCATED BETWEEN STA 500E AND 500F AT S27L CRACKED. REPLACED BAFFLE PER DWG 143A7505 AND AARD 51-00-05.
AIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP LOCATED AT STA 500G AND S27L CRACKED. REPLACED BAFFLE CLIP PER DWG 143A7505 AND AARD 51-00-05.
AIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP LOCATED AT STA 500H AND S27L CRACKED. REPLACED BAFFLE CLIP PER DWG 143A7505 AND AARD 51-00-05.
AIRCRAFT IN BASE MAINTENANCE: BAFFLE CLIP LOCATED AT STA 500H AND S27L CRACKED. REPLACED BAFFLE CLIP PER DWG 143A7505 AND AARD 51-00-05.
AIRCRAFT IN BASE MAINTENANCE: CORROSION OF BAFFLE AT FASTENER HOLES BETWEEN STA 500G AND STA 500H AT STR 27L, MEASURING L=3.0 IN, W=1.0 IN, D=0.01 IN. REPLACED BAFFLE WITH NEW IAW AARD 51-00-05.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HORIZONTAL STABILIZER SKIN LOWER SURFACE HAS A CRACK AT STA 138.7, RIGHT BUTT LINE 101. INSTALLED DOUBLER REPAIR PER SRM 55-10-01-2R.
AIRCRAFT IN BASE MAINTENANCE: BREAK ASSEMBLY PANEL LOCATED AT STA 540 AND RBL 2 TO RBL 22 CRACKED. REPLACED BREAK ASSEMBLY PANEL PER 51-10-20.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN INTERCOSTAL BETWEEN STA 312 AND STA 328 AT RBL 30.5, MEASURING L=1.75 IN, W=0.001 IN, D=0.04 IN. REPLACED INTERCOSTAL WITH NEW IAW AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN INTERCOSTAL BETWEEN STA 328 AND STA 344 AT LBL 45, MEASURING L=1.0 IN, W=0.001 IN, D=0.04 IN. REPLACED INTERCOSTAL WITH NEW IAW AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CORROSION OF FLOORBEAM AT STA 947 AND LBL 16, MEASURING L=32.0 IN, W=1.5 IN, D=0.053 IN. ACCOMPLISHED PERMANENT REINFORCING REPAIR OF FLOORBEAM WITH NESTED ANGLES IAW SRM 53-70-51-2R-5.
AIRCRAFT IN BASE MAINTENANCE: BREAK ASSEMBLY PANEL LOCATED AT STA 540 AND LBL 2 TO LBL 22 CRACKED. REPLACED BREAK ASSEMBLY PANEL PER 51-10-20.
AIRCRAFT IN BASE MAINTENANCE: CORROSION OF SHIELD BETWEEN STA 847 AND STA 867 AT RBL 25, MEASURING L=1.75 IN, W=1.5 IN, D=0.022 IN. REPLACED SHIELD WITH NEW IAW SRM 53-60-15.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON TRANSITION PANEL LOCATED BETWEEN STA 767 AND STA 787 AT RBL 25. REPLACED TRANSITION PANEL PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CORROSION IN AFT OUTBOARD GIRT BAR FASTENER HOLE ON FLOOR BEAM LOCATED AT STA 986.5 AT LBL 48. REPAIRED PER EA 329506 AND SRM 53-70-51-2R-6.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM LOCATED AT STA 986 AND RBL 43.5, MEASURING L=1.00 IN, W=1.00 IN, D=0.095 IN. REPAIRED PER SRM 53-00-51-2R-1 AND EA 329502.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING VERTICAL PRESSURE DECK WEB LOCATED AT STA 663.75 BETWEEN LBL 31.83 AND LBL 40. REPAIRED PER SRM 57-10-10-2R-3 ALT 1.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON TRANSITION PANEL LOCATED BETWEEN STA 727G AND STA 767 AT RBL 25. REPAIRED PER SRM 53-60-01-2 DWG 146A7502 AND SRM 51-40-02 AND AARD 51-00-05.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND TRANSITION PANEL LOCATED BETWEEN STA 500 AND STA 500I AT S23L, LBL 35. REPAIRED PANEL PER SRM 53-00-53-2R-5 AND SRM 51-40-02.
AIRCRAFT WAS NOT GROUNDED: AT FLIGHT LEVEL 360 CAPTAIN LOST INDICATED AIR SPEED MC ENGINE LIGHT ILLUMINATED AFTER SEVERAL MINUTES INDICATED AIR SPEED RETURNED AND MC ENGINE LIGHT WENT OUT. FLIGHT DIVERTED TO DFW ON ACCOUNT OF FAULT. EMERGENCY WAS NOT DECLARED AND POSSIBLY OVERWEIGHT FOR LANDING. CHANGED LEFT PITOT AIR DATA MODULE PER AMM 34-21-04.
AIRCRAFT WAS GROUNDED. AIRSPEED GAVE ERRONEOUS INDICATION ON CLIMBOUT ACCOMPANIED BY AIRSPEED LOW AURAL WARNING. LASTED 1 TO 2 SECONDS ONLY THEN NORMAL. OAT WAS 5 DEGREES, ENGINE ANTI ICE ON, PROBE HEATERS ON, VIS MOISTURE. 13000 FEET STANDBY AIRSPEED WAS 300 KTS. NR 2 WAS 300 KTS. PRIMARY WENT BELOW 150 KTS. FOUND MM 22-11378, LEFT ADIRU FAULT. REMOVED AND REPLACED ADIRU, IAW AMM 34-21-01.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LENS ABOVE R1 DOOR FELL OFF. DUE TO BROKEN PLASTIC LATCHES REPLACED EMERGENCY EXIT SIGN L1063, PER AMM 33-51-01.
AIRCRAFT WAS NOT GROUNDED. IN FLIGHT OVERHEAD LAVATORY SMOKE ANNUNCIATOR LIGHT ILLUMINATED. AFT LAVATORY NO SMOKE OR FUMES NOTED BY FLIGHT ATTENDANTS AFTER PASSENGER EMERGED FROM USE. ACCOMPLISHED LAVATORY SMOKE DETECTOR TEST, PER AMM 26-14-00. OPERATIONS CHECKS NORMAL.
AIRCRAFT WAS GROUNDED: NUMBER 2 FLIGHT DIRECTOR INTERMITTENT. AUTOPILOT B WONT STAY ENGAGED. STAB OUT OF TRIM FLASHES. REMOVED AND REPLACED FLIGHT CONTROL COMPUTER B, DUE TO PHYSICAL EVIDENCE OF DAMAGE ON FRONT CORNERS, PER AMM 22-11-33. ALL RELATED TEST PASSED AND CORRECT SOFTWARE INSTALLED.
AIRCRAFT WAS NOT GROUNDED: DURING TAKEOFF AND CLIMB, CAPTAIN'S FLIGHT DIRECTOR IS NOT PROVIDING INFO OR IS UNDEPENDABLE, SYSTEM SELF-CORRECTS ABOVE APPROXIMATELY 3,000-4,000 FT. FLIGHT DIRECTOR DEFERRED ON MEL 34-07B FOR CONTINUED OPERATION. REPLACED FCC-B WITH NEW IAW AMM 22-11-33, OPS CHECK GOOD.
AIRCRAFT WAS GROUNDED: FLAP LEVER BINDING OR DIFFICULT TO MOVE AT POSITION FLAP 1 AND FLAP POSITION 15 GATE. ACCOMPLISHED FIM TASK 27-51-00-810-843 FLAP LEVER OPERATES NORMALLY NO BINDING OR DIFFICULTEY MOVING.
AIRCRAFT NOT GROUNDED: UNABLE TO TRANSMIT ON HF2 AND ATTEMPTING TO TRANSMIT ON HF1 AND ARINC HAD DIFFICULTY HEARING US. BOTH HF RADIOS NEED TO BE CHECKED.***SUPPLEMENTAL ACTION SECT. 4 AND 5: REMOVED AND REPLACED HF#1 AND HF#2 ANTENNA. COUPLERS IAW AMM 23-11-61.ALSO SEE AALA202001249006***(CLOSED)
AIRCRAFT NOT GROUNDED: UNABLE TO TRANSMIT ON HF2 AND ATTEMPTING TO TRANSMIT ON HF1 AND ARINC HAD DIFFICULTY HEARING US. BOTH HF RADIOS NEED TO BE CHECKED.***SUPPLEMENTAL ACTION SECT. 4 AND 5: REMOVED AND REPLACED HF#1 AND HF#2 ANTENNA. COUPLERS IAW AMM 23-11-61.ALSO SEE AALA202002049001***(CLOSED)
AIRCRAFT WAS GROUNDED: PILOT REPROTS IN CLIMB @ FL 250, AMBER L.E. IN TRANSIT LIGHT ILLUMINATED INTERMITTANTLY. DID QRH PROCEDURES UPON APPROACH TO MIA WITH FLAPS EXT. LIGHT CONTINUED TO FLASH EVEN W/ 15 FLAPS. MAINTENANCE FOUND SL6 PROX OUTBOARD MSG 27-81210 DISPLAYED ON FSEU. REMOVED AND REPLACED SLAT #6 OUTBOARD PROXIMITY SENSOR IAW AMM 27-88-11. OPS CHECK OKAY.
AIRCRAFT WAS NOT GROUNDED: DURING WALK AROUND FOUND DOOR 1R SLIDE LAMP INOPERATIVE. SUPPLEMENTAL TO UPDATE SECTION 4 AND SECTION 5. MAINTENANCE REPLACED BATTERY PACK PER AMM 33-51-06. (CLOSED)
AIRCRAFT WAS GROUNDED: PILOT REPORTS UPON ROTATION, LOST CA HUD AND PFD FLIGHT DIRECTOR SYMBOLOGY. FO LOST SYMBOLOGY ALSO FD SYMBOLOGY. RETURNED AT APPROX. 1000FT AFL. MAINTENANCE REPLACED ADIRU-2 IAW AMM-34-21-01. OPS CHECKS GOOD. DFCS OPS GOOD IAW AMM-22-11-00.
AIRCRAFT WAS NOT GROUNDED: EXIT SIGN FELL OFF THE LEFT AFT ENTRY DOOR. MAINTENANCE REPLACED SIGN PER AMM 33-51-00.
AIRCRAFT NOT GROUNDED: PILOT REPORTS BOTH FLIGHT DIRECTORS BLANK OUT ON TAKEOFF MOMENTARILY, CA RETURNED, FO STAYED BLANK. NO FAULTS NOTED. RIGHT IRS HAD NO POSITION AIRBORNE BUT NO FAULT LIGHT. FO FLIGHT DIRECTOR RETURNED AFTER ENTERING HDG FOR FO. MAINTENANCE REPORTS FFR SHOWS ADIRU(IRU) FAULT #2. MSG 22-11006. ACCOMPLISHED FIM 22-11-00-810-807, ALL CHECKS NORMAL. DFCS BITE CHECK NORMLA. IRU AND FD SYSTEMS CHECK NORMAL.
AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING FLAP EXTENSION, FLAPS STUCK BETWEEN 15 AND 25. L/E LIGHTS AGREED WITH TRAILING EDGE POSITION. FLAPS LEFT DOWN AT GATE FOR INSPECTION. MAINTENANCE ACCOMPLISHED TASK IAW FIM 27-51-00-810-849. NO FAULTS NOTED.
AIRCRAFT WAS GROUNDED: FORWARD ENTRY DOOR UPPER PRESSURE STOP FITTING BEARING PAD BROKEN. REPLACED PRESSURE STOP FITTING BEARING PAD PER AMM 52-11-01.
BOTH AFT SLIDES HAD MATERIAL HANGING OUT OF THE BUSTLE. MAINTENANCE RESTOWED THE R2 DOOR SLIDE MATERIAL, AND ATTACHED TO THE HOOK AND LOOP IAW AMM 25-66-01. PERFORMED A SATISFACTORY OPERATIONAL CHECK.
DURING A PREFLIGHT, THE L1 FLASHLIGHT WAS FOUND INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD, OK FOR SERVICE.
AIRCRAFT WAS NOT GROUNDED. DURING 2908 WORKCARD, RIGHT HAND SIDE OF AIRCRAFT ROWS 15-22 UPPER EMERGENCY LIGHTS WENT OUT. REPLACED BATTERY PACK PAC5026 AT POSITION M1695 AS PER AMM 33-51-06. OPERATIONS CHECKS NORMAL.
AIRCRAFT WAS NOT GROUNDED. DURING 2908 WORKCARD, ROW 15DEF EMERGENCY SIDEWALL LIGHT WENT OUT. REPLACED BATTERY PACK PAC5026 AT POSITION M1694 AS PER AMM 33-51-06. OPERATIONS CHECKS NORMAL.
AIRCRAFT WAS NOT GROUNDED. DURING 2908 WORKCARD, LEFT HAND SIDE OF AIRCRAFT ROWS 12-30 LOWER AND UPPER EMERGENCY LIGHTS WENT OUT. REPLACED BATTERY PACK PAC5026 POSITION M1671 AS PER AMM 33-51-06. OPERATIONS CHECKS NORMAL.
AIRCRAFT WAS NOT GROUNDED. DURING 2908 WORKCARD, R2 DOOR EMERGENCY LIGHTS WENT OUT. REPLACED BATTERY PACK PAC5026 POSITION M1670 AS PER AMM 33-51-06. OPERATIONS CHECKS NORMAL.
AIRCRAFT WAS NOT GROUNDED. THRESHOLD LIGHT NEAR FLOOR AT L1 DOOR HAS A DETACHED LENS COVER. REPLACED LIGHT IAW AMM 33-14-00. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED. WHEN THROTTLES ADVANCED FOR TAKEOFF, THE TAKEOFF CONFIGURATION WARNING SOUNDED. RETURNED TO GATE. REMOVED AND REPLACED RIGHT FLAP POSITION TRANSMITTER ASSEMBLY IAW AMM 27-58-01. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY DECLARED. ON FINAL APPROACH, FLAPS SPLIT AT 10 1.5 DEGREES AND DID NOT MOVE. UNEVENTFUL LANDING. ACCOMPLISHED ALTERNATE FLAP MOVEMENT PROCEDURE. ACCOMPLISHED FUNCTIONAL TEST AND FSEU BITE PROCEDURE. FAULT CLEARED WITH NO CURRENT FAULTS. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY DECLARED. MISSED APPROACH EXECUTED ACCOUNT FLAPS DID NOT EXTEND. ALTERNATE FLAP EXTENSION UTILIZED AND LANDING UNEVENTFUL. INSPECTED FLAPS, FLAP TRACKS, FLAP SKEW SENSORS AND RAN FLAPS WITH NO ISSUES NOTED. ACCOMPLISHED FSEU BITE IAW FIM 27-51-00-810-801. OPERATIONAL CHECK GOOD.
AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN AT L4 DOOR HAS A DETACHED LENS COVER. REATTACHED LENS COVER. OPERATIONAL CHECK GOOD.
L1 DOOR EMERGENCY EVACUATION SLIDE BALL DISENGAGED FROM BRACKET. SEATED THE SLIDE PACK AND COVER IAW AMM 25-66-01. OPERATIONAL CHECKED GOOD.
LENS LOOSE ON FORWARD EMERGENCY FLOOD LIGHT AT G2 GALLEY SIDEWALL. REPLACED FORWARD GALLEY ENERGENCY FLOOD LIGHT ASSEMBLY IAW AMM 33-51-14, CHECKED OK IAW AMM 33-51-00. THE AIRCRAFT WAS NOT GROUNDED.
CENTER WING SUPPORT BEAM HAS WORN AREA CAUSED BY A WORN OUT DOOR STOP ON PNEUMATIC AIR ACCESS DOOR 192DR. REPAIRED CTR WING SUPPORT BEAM IAW EA 252612.
CABIN SEAT TRACK BOLT HOLE CRACKED AT RBL 45.50. REPAIR ACCOMPLISHED IAW EA 252764 DATED 07 15 2015 & ECO J1707BA CA.
CABIN SEAT TRACK BOLT HOLE CRACKED AT LBL 45.50. REPAIR ACCOMPLISHED IAW EA 252764 DATED 07 15 2015 & ECO J1707BA CA.
CABIN SEAT TRACK BOLT HOLE CRACKED AT RBL 24.75. REPAIR ACCOMPLISHED IAW EA 252764 DATED 07 15 2015 & ECO J1707BA CA.
CABIN FLOOR INTERCOSTAL AT BL 0 BETWEEN FS 294 & 303 IS CRACKED. R & R INTERCOSTAL IAW AARD 51-00-05-1.
CORROSION FOUND ON G4 GALLEY WALL SUPPORTED 147A5710-1 2. R & R LT & RT G4 GALLEY WALL SUPPORT 147A5710-1 2 IAW SRM 51-10-2 PAR 8.
CORROSION FOUND ON G4 GALLEY WALL SUPPORTED 147A5710-1 2. R & R LT & RT G4 GALLEY WALL SUPPORT 147A5710-1 2 IAW SRM 51-10-2 PAR 8.