N78511

Service difficulty reports · 48

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N78511' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026060116713Drive Unit · faultedWXR FAIL BOTH SIDES WXR FAIL ATTN REF LP 9066608 FOR MAINTENANCE ACTION PERFORMED. LP 9066608: DUE TO HISTORY OF PWS AND WX INOP, PLEASE CHANGE WX DRIVE UNIT. . RAR WX DRIVE UNIT. REF AMM 34-43-11/401. INSTALLATION OPS CHECK WILL STILL NEED TO BE PERFORMED. May 27, 2026 · N78511 · Boeing 737824 · Weather Radar SystemSDR CALA2026042415702Release Mech · brokenFWD DOOR SLIDE GIRT BAR STOP RELEASE BROKEN. L1 DOOR. PART AOG. REMOVED AND REPLACED GIRT BAR STOP IAW IPC 25-66-00-13.Apr 24, 2026 · N78511 · Boeing 737824 · Escape SlideSDR CALA2026041715454Skin · damagedPOSSIBLE LIGHTNING STRIKE DAMAGE AT STATION 221 APROX 16 INCHES ABOVE THE LAP SEAM ON FO SIDEBEGAN LAYING OUT FASTENERS IN RELATION TO DAMAGE. DOES NOT QUALIFY FOR DRILL OUT REPAIR AS IT DOES NOT MEET REQUIREMENT 1 D 1 F OF SRM 53-00-01-2R-38, NOT MORE THAN 4Apr 10, 2026 · N78511 · Boeing 737824 · Fuselage Main, Plate/SkinSDR CALA2026040815188Door Latch · wornRIGHT FWD LATCH FOR DOOR 192 DR HAS WORN INTO CHORD ALMOST ALL THE WAY THROUGH.MARKED MAJOR REPAIR AND INITIATED SFR. INITIATED SDR REMOVED DOOR 192 DR, ECS DOOR SEAL AND RETAINER FOR ACCESS TO SHEETMETAL REPAIR.REF SRM 57-10-13-2R-3. STEP 4A. COMPLIED WITH SApr 2, 2026 · N78511 · Boeing 737824 · DoorsSDR CALA2026012613298Door · no discrepancyFLT ATT STATE THE DOOR SLIDE 1L ISN`T ARMING NORMALLY DOOR 1L ARMED NORMALLY NO PROBLEM FOUNDJan 26, 2026 · N78511 · Boeing 737824 · Cabin Equipment/FurnishingsSDR CALA2025062005740Unknown · odorFA REPORTS BRAKE FLUID LIKE ODOR IN AFT LAV D ACP ENGINE RUN AND RAN PACKS , COULD NOT DUPLICATE SMELL IN CABIN. FLIGHT ATTENDANT REPORTED SMELL WENT AWAY IN FLIGHT.Jun 19, 2025 · N78511 · Boeing 737824 · Air Distribution SystemSDR CALA2025052805027Unknown · odorSMOKE SMELL IN CABIN NEAR 38F. DEBRIEFED FLIGHT CREW. PILOTS REPORTED THAT THE SCENT WAS NOTICED ONLY AFTER PACK 2 WAS BEING POWERED BY ENGINE 2 BLEED AIR. NO SCENT WAS REPORTED WHEN APU BLEED POWERED BOTH PACKS. OPENED FAN COWLS. INSPECTED E2 FOR FLUID LEAKMay 26, 2025 · N78511 · Boeing 737824 · Air Distribution SystemSDR CALA2025052805052Latch · disengagedRTO 60 KIAS DOOR LIGHT FWD ENTRY FA HAD NOT LATCHED DOOR ALL YH E WAY PERFORMED FWD ENTRY DOOR GVI, OPEN AND CLOSE OPERATION NORMAL REF AMM 52-11-00. DUE TO LOW ENERGY STOP PERFORMED GVI OF BRAKES, LANDING GEAR AND TIRES WITH NO DEFECTS NOTED.May 24, 2025 · N78511 · Boeing 737824 · Passenger/Crew DoorsSDR CALA2025031002669Lamp · inoperativeEMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - EMER EXT LIGHT AT 2L DOOR INOP. RELAMPED ONE EMER EXT LIGHT AT 2L DOOR REF IPC 33-51-04-06A, OPS CHECK OK.PARTS USED: 99-3351-3-0014,QTY :1Mar 8, 2025 · N78511 · Boeing 737824 · Emergency LightingSDR CALA2025022402458Warning Message · intermittentRIGHT AFT OVERWING DOOR CAUTION LIGHT ON DURING T/OFF. RTO AT 73 KTS FOUND FAULT MESSAGE 52-72008 IN FLIGHT LEG 0 HISTORY PERFORMED INITIAL EVALUATION PER FIM 52-20 TASK 801, PERFORMED P ROXIMITY SWITCH ELECTRONICS UNIT (PSEU) BITE PROCEDURE, 32-09 TA SK 801 NFeb 20, 2025 · N78511 · Boeing 737824 · Door Warning SystemSDR CALA2025010201751Windshear Sys · faultedWINDSHEAR ALERT ON T/O SUSPECT ARCFT SYSTEM FAULT. SEEMS TO HAPP EN ABOVE 50ISH PERCENT N1. PERFORMED BITE CHECK ON WXR RADAR SYSTEM NO FAULTS FOUND. SUSPECT PROBLEM IN A/T SWITCH PACK. PLACED AUTOTHROTTLE ON MEL 2204A. PERFORMED BITE CHECK ON WXR RADAR SYSTDec 27, 2024 · N78511 · Boeing 737824 · Wind Shear Detection SystemSDR CALA2024090600592Flap System · malfunctionedON APP FLAP ASSYMETRY WHEN SEL F25. TURNED INTO A FLAP DISS F15- 25 AFTER LNDG FLAPS SHOW15 AHM UPDATE: CHIME ALERT FOR THE BYPASS. PERFORMED FSEU BITE. LAST LEG FAULT HISTORY SHOWED TE FLAPS SNSR DIS FAULT CODE 27-52261. CURRENT FAULTS SHOWED FLAP LEVER FASep 6, 2024 · N78511 · Boeing 737824 · Trailing Edge Flap Control SystemSDR CALA2024090502390Flap System · faultedON APP FLAP ASSYMETRY WHEN SEL F25. TURNED INTO A FLAP DISS F15- 25 AFTER LNDG FLAPS SHOW15 AHM UPDATE: CHIME ALERT FOR THE BYPASS. SEE ATTACHED REPORT. PERFORMED FSEU BITE. LAST LEG FAULT HISTORY SHOWED TE FLAPS SNSR FIM REF 27-51 TASK 819 RECOMMENDS CHANGINGSep 4, 2024 · N78511 · Boeing 737824 · Trailing Edge Flap Control SystemSDR CALA2024083000517Motor · faultyELEC PITCH TRIM INOP DUR ING CLIMB MSG PHOTO UPDATE ACP FIM 27-41 TASK 805. RESET CB'S ,STM LOGIC RESET. STAB GRD CHKS NORMAL PER REPAIR CONFIRMATION ADD EMP:U159655 PICS UPDATE FOT SPEED/ STAB TRIM , SURFACE AND LAND VERFIED TEST ALL PASSED PER TOMC REMOVE ANAug 28, 2024 · N78511 · Boeing 737824 · Stabilizer Position IndicatingSDR CALA2024072902124Skin · crackedCRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN STAB STA 92.70,11.5 INCHES FROM REAR SPAR I/B ROW.CRACK LENGHT 0.343 INCHES. REF. AAR N/R:9894470 55-10-01-2R11 TABLE 204. 9000 FLIGHT CYCLE INTERVALS AND 56000 THRESHOLD. SKIN REPAIR ACCOMPLISHED ON RIGHT HORJul 12, 2024 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2024071502040Support · crackedFWD CABIN WET AREA L-1 CUTOUT FWD LOWER SILL INNER CHORD CRACKED AT SUPPORT FRAME ATTACHMENT FASTENER HEAD STA 303.9 LBL 59 REF. AAR N/R:9894904Jul 12, 2024 · N78511 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2022102802990Detector · faultedENGINE #1 FIRE TEST DOES NOT WORK LIMITS. NEXT CHECKED RESISTANCE OF FIRE DETECTOR LOOP B, DISCONNECTED AFT TERMINAL LUG, CHECKED RESISTANCE AT DETECTOR TO GND, RESISTANCE IN LIMITS. REQUEST DEFERRAL DEFERRED TOMC APPROVED FOR MEL 2602C ENGINE #1 FIRE TEST DOOct 28, 2022 · N78511 · Boeing 737824 · Detection SystemSDR CALA2022011700162Light · illuminatedRIGHT AFT OVERWING LIGHT ILLUMINATED WHEN THRUST LEVERS WERE ADV ANCED PSEU SHOWS FAULT CODE 52-72008. REF FIM 52-20 TASK 801 INITIAL EVALUATION SHOWS FAULT WAS INTERMITTENT. PSEU LIGHT AND RIGHT OVERWING EXIT LIGHTS BOTH EXTINGUISHED DURING FIM EVALUATION PROJan 16, 2022 · N78511 · Boeing 737824 · DoorsSDR CALA2021112902174Door · unsecureUNUSUAL VIBRATION FELT ON CLIMBOUT AT FL200 AND ABOVE..290-300KT S COMING FROM COCKPITFLOOR ON WALK AROUND FOUND EXT POWER DOOR NOT SECURED, CLOSED DOOR AND CHECKED SECURITY. NO ISSUES NOTED. PER FIM TASK 05-51-04-210-801 UNUSUAL VIBRATION INSPECTION. C/WNov 29, 2021 · N78511 · Boeing 737824 · DoorsSDR CALA2021080901302Skin · corrodedPOSSIBLE INTERIOR SKIN CORROSION ON WASH, SKIN AND RIVETS BUCKLED FROM STA 360 TO STA 400 AROUND S-26 LEFT APPROX. [EXTERIOR SKIN CIRCLED] FLEET CYCLE LOG PAGE 9780955. INITIATE A 2ND DTA DIP FOR "PLANNING TO CONTACT ENGINEERING AFTER 16 MONTHS, BUT BEFORE 17 Aug 9, 2021 · N78511 · Boeing 737824 · Fuselage Main, Plate/SkinSDR CALA2021080901296Skin · crackedCRACK ON LOWER INSPAR SKIN ON RIGHT HORIZONTAL STAB STA.175.5 " 16" FROM FORWARD SPAR AND MEASURING .75" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780724 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FIG Aug 6, 2021 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2021080901295Skin · crackedCRACK ON LOWER INSPAR SKIN ON RIGHT HORIZONTAL STAB STA.147.9 " 27.5" FROM FORWARD SPAR AND MEASURING 1.5" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780721 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FIAug 6, 2021 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2021080901294Skin · crackedCRACK ON LOWER INSPAR SKIN ON LEFT HORIZONTAL STAB STA.193.5 " , 27" FROM FORWARD SPAR AND MEASURING 1.25" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780720 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FIAug 6, 2021 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2021080901293Skin · crackedCRACK ON LOWER INSPAR SKIN ON LEFT HORIZONTAL STAB STA.129.50 " 27.5" FROM FORWARD SPAR AND MEASURING 1.0" IN LENGTH . LOG PAGE FOR DIP ENTRY ONLY, SEE FLEET CYCLE L/P 9780718 FOR REP INST PER SRM 55-10-01-2R-11. NEED TO PERFORM INSP AS GIVEN IN TABLE 204 & FIAug 6, 2021 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2021080901290Skin · corrodedPOSSIBLE INTERIOR SKIN OR STRINGER CORROSION BETWEEN STA 360 TO STA 400 AROUND S-25 LEFT APPROX. [MARKED ON SKIN IN RED] FLEET CYCLE LOGPAGE #9781175. INITIATE A DTA DIP TO "ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS FROM AUGUST 2, 2021." NOTE TO PLANNING:Aug 6, 2021 · N78511 · Boeing 737824 · Fuselage Main, Plate/SkinSDR CALA2021080901288Skin · corrodedPOSSIBLE INTERIOR SKIN CORROSION NOTICED ON WASH, SKIN AND RIVETS BUCKLED FROM STA 360 TO STA 400 AROUND S-26 LEFT APPPROX. [EXTERIOR SKIN CIRCLED] FLEET CYCLE LOG PAGE 9780955. INITIATE A DTA DIP TO "ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS FROM JULY 29Aug 6, 2021 · N78511 · Boeing 737824 · Fuselage Main, Plate/SkinSDR CALA2020041000822Anti-Skid Valve · out of toleranceANTISKID INOP LIGHT LIGHT ON PER FIM TASK 32-42-00-810-803 BOX 1-4. FOUND VALVE 4 V10 OUT OF TOLERANCE. VALVE PART NO. 37-231. NEEDS TO BE REPLACED. SSM 32-41-11 REF. REQ''S PN 39-353, REF: IPC 32-42-31-02 ITEM 330. (M&E# 99-3249-9-0001). REMOVED & REPLACED R/Apr 10, 2020 · N78511 · Boeing 737824 · Brake Anti-Skid SectionSDR CALA2018083101863Skin · corrodedCORROSION ON FUSELAGE SKIN SURFACE APPROXIMATELY BETWEEN STA 287 & STA 289 JUST ABOVE STR 23L. REF. FLEETCYCLE LOG PAGE 9612801. CUT OUT DAMAGED AND INSTALLED REPAIR DOUBLER PER SRM53-00-01 REPAIR 3 AND ECRA5330-06419. REI NSPECT PER SRM 53-00-01 TABLE 205 ANDAug 27, 2018 · N78511 · Boeing 737824 · Fuselage Main, Plate/SkinSDR CALA2018082001819Floorbeam · corrodedCORROSION FOUND ON THE FLOORBEAM, BS 328, RBL 58. REPAIRED THE FLOORBEAM IAW SRM 53-10-51, REPAIR 7.Aug 16, 2018 · N78511 · Boeing 737824 · Fuselage Main, Floor BeamSDR CALA2018081701798Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SURFACE CRACKED AT THE LOWER INSPAR SKIN AT HSS 147.90 & 11 INCHES FROM THE REAR SPAR. FABRICATED A REPAIR IAW SRM 51-10-01, REPAIR 11.Aug 10, 2018 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2017061801873Battery Pack · failedMOST EMERGENCY LIGHTS FAIL CAPACITY CHECK PER W/C 29-3350-1-7100 . REPLACED BATTERY PACKS AT THE FOLLOWING EMERGENCY LIGHTS POWER SUPPLIES IAW AMM 33-51-06: M1674 M1676 M1694 M1695 M1670 M1671 M1673 M1672. CAPACITY AND FUNCTIONAL CHK GOOD IAW AMM 33-51-0Jun 18, 2017 · N78511 · Boeing 737824 · Emergency LightingSDR CALA2016012800076Engine · fireFLIGHT ATTENDANT REPORTED LOUD BANG FROM LT ENG AS POWER WAS BEING APPLIED ON TAKEOFF ROLL. ACFT BEHIND REPORTED SEEING FLAME FROM LT ENG. NO ABNORMAL INDICATIONS ON COCKPIT GAUGES. ACCOMPLISHED AMM 71-00-00-210-801-F00 & FIM 71-05-00-810-805-F00 STEPS 1 - Jan 28, 2016 · N78511 · Boeing 737824 · Engine (Turbine/Turboprop)SDR CALA2015092100781Seat Track · crackedPERFORMED HFEC INSPECTION OF THE FOUR INDICATED SEAT TRACK FASTENER HOLES IAW NDT PART 6 51-00-00 PROCEDURE 16, AT LBL 24.75. FOUND CRACK INDICATION ABOVE 50% OF SCREEN HEIGHT ON FASTENER LOCATIONS 1, 3 & 4. REPAIRED FASTENER HOLES IAW ECRA 5320-02586.Sep 19, 2015 · N78511 · Boeing 737824 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2015092100780Seat Track · crackedPERFORMED HFEC INSPECTION OF THE FOUR INDICATED SEAT TRACK FASTENER HOLES IAW NDT PART 6 51-00-00 PROCEDURE 16, AT RBL 45.50. FOUND CRACK INDICATION ABOVE 50% OF SCREEN HEIGHT ON FASTENER LOCATION 1. REPAIRED FASTENER HOLES IAW ECRA 5320-02586.Sep 19, 2015 · N78511 · Boeing 737824 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2015092100779Seat Track · crackedPERFORMED HFEC INSPECTION OF THE FOUR INDICATED SEAT TRACK FASTENER HOLES IAW NDT PART 6 51-00-00 PROCEDURE 16, AT RBL 24.75. FOUND CRACK INDICATION ABOVE 50% OF SCREEN HEIGHT ON FASTENER LOCATION 1 & 2. REPAIRED FASTENER HOLES IAW ECRA 5320-02586.Sep 19, 2015 · N78511 · Boeing 737824 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2015092100782Seat Track · crackedPERFORMED HFEC INSPECTION OF THE FOUR INDICATED SEAT TRACK FASTENER HOLES, IAW NDT PART 6 51-00-00 PROCEDURE 16 AT LBL 45.50. FOUND CRACK INDICATION ABOVE 50% OF SCREEN HEIGHT ON FASTENER LOCATIONS 1 & 2. REPAIRED FASTENER HOLES IAW ECRA 5320-02586.Sep 19, 2015 · N78511 · Boeing 737824 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2015091800769Skin · crackedFOUND CRACK ON LT HORIZONTAL STAB LOWER SKIN AT STAB STATION 129.5, 18 1/2" FWD OF AFT EDGE OF SKIN. ADJACENT TO DRAIN HOLE, CRACK IS JUST UNDER 1" LONG. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED IAW SRM 55-10-01 REPAIR 11 PARAGRAPHSep 17, 2015 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2015091800768Skin · crackedFOUND CRACK ON LT HORIZONTAL STAB LOWER SKIN AT STAB STATION 101.9, 11" FWD OF AFT EDGE OF SKIN, CRACK IS 1" LONG. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED IAW SRM 55-10-01 REPAIR LL PARAGRAPH 5 TABLE 204. PERFORM DV & LFEC INSPECTSep 17, 2015 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2015091800774Skin · crackedWHILE PERFORMING C SCAN, FOUND CRACK ON RT HORIZONTAL STAB LOWER SKIN AT STAB STATION 129.5, 10" FWD OF AFT EDGE OF SKIN. CRACK IS APPROX 1" LONG. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED IAW SRM 55-10-01 REPAIR 11 PARA 5,TABLE 204Sep 17, 2015 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2015091800773Skin · crackedWHILE PERFORMING C SCAN, FOUND CRACK ON RT HORIZONTAL STAB LOWER SKIN AT STAB STATION 138.7, 9" AFT OF FWD EDGE OF SKIN. CRACK IS APPROX 3/4" LONG. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED IAW SRM 55-10-01 REPAIR 11 PARA 5, TABLE 2Sep 17, 2015 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2015091800772Skin · crackedWHILE PERFORMING C SCAN, FOUND CRACK ON RT HORIZONTAL STAB LOWER SKIN AT STAB STATION 138.7, 16 3/4" AFT OF FWD EDGE OF SKIN. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED IAW SRM 55-10-01 REPAIR 11 PARAGRAPH 5 TABLE 204. PERFORM DV & LSep 17, 2015 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2015091800771Skin · crackedWHILE PERFORMING C SCAN, FOUND CRACK ON RT HORIZONTAL STAB LOWER SKIN AT STAB STATION 101.9, 11" FWD OF AFT EDGE OF SKIN CRACK. CRACK IS APPROX 3/4" LONG. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED IAW SRM 55-10-01 REPAIR 11 PARA 5 TSep 17, 2015 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2015091800770Skin · crackedWHILE PERFORMING C SCAN, FOUND CRACK ON RT HORIZONTAL STAB LOWER SKIN AT STAB STATION 175.5 10 1/4" FWD OF AFT EDGE OF SKIN. CRACK IS APPROX 3/8" LONG. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED IAW SRM 55-10-01 REPAIR 11, PARAGRAPH Sep 17, 2015 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2015011200036Trim Motor · malfunctionedAT FL360 STAB OUT OF TRIM LIGHT ILLUMINATED. RAN QRH, STAB OUT OF TRIM, CHECKLIST. STAB WAS NOT TRIMMING. STAB DID NOT RESPOND TO ELEC TRIM INPUTS. RAN ELEC TRIM INOPERATIVE. CHECKLIST, CLUTCH WOULD NOT DISENGAGE. TOOK BOTH PILOTS TO FORCE IT TO DISENGAGJan 12, 2015 · N78511 · Boeing 737824 · Stabilizer Position IndicatingSDR CALA2014062300811Unknown · odorSMOKE & FUMES IN FC GALLEY AFTER CHECKLIST, 15 MINUTES FUMES RE-APPEARED ON OPPOSITE SIDE OF FC GALLEY BEHIND CAPTAINS SEAT. PERFORMED TASK 05-51-26-800-801C1 SMOKE ODOR IN CABIN. CONDITIONAL INSPECTION SUSPECT OVEN 205 FC CABIN, OTHERWISE NO SIGNIFICANT FINJun 23, 2014 · N78511 · Boeing 737824 · Air Distribution SystemSDR CALA2013021400109Skin · crackedLT HORIZ STAB LOWER SKIN AT HSS 138.70 BETWEEN THE 8TH AND 9TH RIVETS AFT OF FRONT SPAR INBD ROW SHOWS CRACK INDICATION LT STAB LOWER SKIN AT HSS 138.70 HAS BEEN REPAIRED IAW SRM 55-10-01, REPAIR 11.Feb 12, 2013 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2013021100089Skin · crackedRT HORIZ STAB LOWER SKIN AT STA 147.90 BETWEEN THE 7TH AND 8TH RIVET FROM THE AFT SPAR INBD ROW SHOWS CRACK INDICATION RT STAB LOWER SKIN AT STA 147.90 HAS BEEN REPAIRED IAW SRM 55-10-01, REPAIR 11 REINSPECT AT 56,000 FLT CYC''S AFTER REPAIR BY DVI AND LFEC TEFeb 11, 2013 · N78511 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2011041500288Unknown · odorSTRONG SMELL OF PLASTIC BURNING JUST AFTER TAKEOFF. UPON ARRIVAL DEBRIEFED CREW AND FOUND SMELL HAD DISSIPATED BEFORE RETURN TO EWR. PERFORMED IMMEDIATE INSPECTION OF LP PLENUM ( WHERE GROUND AIR CONDITION HOOKS UP) FOUND NO OIL RESIDUE. PERFORMED FIMTASK 21Apr 15, 2011 · N78511 · Boeing 737824 · Air Distribution System
Back to N78511