Boeing 737-83N

Service difficulty reports · 1,087

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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 aircraft_model_key = '73783N'
  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 UIEA2025061200742Channel · corrodedAFT CARGO COMP RAIL-CHANNEL LBL 8.10 CORROSION NOTED BETWEEN STA 787 TO STA 767.(<P>REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL LBL 8.10 BETWEEN STA 787 TO STA 767 +5" IAW SRM 51-10-02 REV 23. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.032", FOUND TJun 11, 2025 · N5179A · Boeing 73783N · Fuselage Miscellaneous StructureSDR UIEA2025061200745Channel · corrodedAFT CARGO COMP RAIL-CHANNEL RBL 8.10 CORROSION NOTED BETWEEN STA 787 TO STA 767.(<P>REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL RBL 8.10 BETWEEN STA 787 TO STA 767 +4" IAW SRM 51-10-02 REV 23. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.042", FOUND TJun 11, 2025 · N5179A · Boeing 73783N · Fuselage Miscellaneous StructureSDR UIEA2025061300759Skin · crackedRH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 120.30 +10" FROM AFT SPAR, CRACK LENGTH 1.25".(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.090" AND FILLER REPAIR ALUMINUM 2024-T3 0.071" AT RH HORIZONTAL STABILIZER, LOWER SKINJun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025061300760Skin · crackedRH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 129.50 +34.25" FROM AFT SPAR, CRACK LENGTH 1.0".(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.080" AND FILLER REPAIR ALUMINUM 2024-T3 0.063" AT RH HORIZONTAL STABILIZER, LOWER SKJun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025061300761Skin · crackedLH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 120.30+10" FROM AFT SPAR, CRACK LENGTH 1.0".(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.090" AND FILLER REPAIR ALUMINUM 2024-T3 0.071" AT LH HORIZONTAL STABILIZER, LOWER SKIN SJun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025061300762Skin · crackedLH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 129.50+26" FROM AFT SPAR, CRACK LENGTH 1.0".(<P>ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.080" AND FILLER REPAIR ALUMINUM 2024-T3 0.063" AT LH HORIZONTAL STABILIZER, LOWER SKIN SJun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025061300763Channel · corrodedAFT CARGO COMP RAIL-CHANNEL RBL 3.00 CORROSION NOTED BETWEEN STA 787 TO STA 767.(<P>REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL RBL 3.00 BETWEEN STA 787 TO STA 767 +5" IAW SRM 51-10-02 REV 23. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.045", FOUND TJun 11, 2025 · N5179A · Boeing 73783N · Fuselage Miscellaneous StructureSDR UIEA2025061300764Floorbeam · corrodedMDCC, FLOOR STRUCTURE, BS 986.5 BETWEEN LBL 24.75 TO L2 DOOR INNER CHORD WITH SURFACE CORROSION.(<P>PERFORMED PERMANENT REPAIR AT TRANSVERSAL FLOOR BEAM STA 986.5 BTW BL 0.00 AND LBL 50.00 UPPER HORIZONTAL FLANGE AS PER ENGINEERING ORDER CONTROL #25101-1 REV AJun 11, 2025 · N5179A · Boeing 73783N · Fuselage Main, Floor BeamSDR UIEA2025061300765Rib · crackedDURING VISUAL INSPECTION OF RH HORIZONTAL STABILIZER IN THE INSPAR RIB, LOWER CHORD STAB STA 92.70 WERE FOUND 2 CRACKS AT STIFFENER #2 AND STIFFENER #3.(<P>ACCOMPLISHED CATEGORY "A" REPAIR, PERMANENT REPAIR ON R/H HORIZONTAL STABILIZER INSPAR RIB STA 92.70 AT Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/RibSDR UIEA2025061300766Rib · crackedCRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 95.96.(<P>REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 95.96 AND INSTALLED SAME RIB CHORD (PN 186A1303-2) L/E STA 95.96 AS PER SRM BCG-D634A209 AND 51-40-02-0G-0 REV 23. NO FURTHERJun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/RibSDR UIEA2025061300767Rib · crackedCRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 105.26.(<P>REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 105.26 AND INSTALLED SAME RIB CHORD L/E STA 105.26 (PN 186A1304-2) AS PER SRM BCG-D634A209 AND SRM 51-40-02-0G-0 REV 23. NO Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/RibSDR UIEA2025061300768Tail Cone · dentedREF DMI #194100: PERFORM PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM SECTION.(<P>PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM SECTION WAS ACCOMPLISHED BY OUTSIDE VENDOR SAL AEROSPACE TECHNOLOGIES W/O #400100088. NO FURTHER DEFEJun 11, 2025 · N5179A · Boeing 73783N · Aerodynamic FairingsSDR UIEA2025061300769Rib · crackedCRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 114.55.(<P>REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 114.55 AND INSTALLED SAME RIB CHORD (PN 186A1305-1) L/E STA 114.55 AS PER SRM BCG-D634A209 AND SRM 51-40-02-0G-0 REV 23. NO Jun 11, 2025 · N5179A · Boeing 73783N · Horizontal Stabilizer, Spar/RibSDR UIEA2025061300770Panel · corrodedCOVER OF AFT BULKHEAD OF FWD CARGO COMPARTMENT, INTERNAL SQUARE WITH CORROSION ON HOLES FOR FASTENERS.(<P>UPON EVALUATION ON FWD CARGO AFT BULKHEAD PANEL WAS FOUND TO BE OUT OF LIMITS PER SRM 51-10-02-0G-0. REMOVED AND REPLACED PANEL AS REQUIRED PER 25-52-17-4Jun 11, 2025 · N5179A · Boeing 73783N · Fuselage Main, StructureSDR UIEA2025061300771Battery Pack · inoperativeRH SIDE EMERGENCY LIGHTS INOP.(<P>REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 REV 86. OPERATIONAL TEST SATISFACTORY.</P>)Jun 11, 2025 · N5179A · Boeing 73783N · Emergency LightingSDR SCNA20250606199Slide · dislodgedUPON OPENING L-1 DOOR EMERGENCY ESCAPE SLIDE FELL OUT OF BUSTLE CONTAINER - RESOLUTION: INSTALLED NEW L1 DOOR SLIDE IAW AMM 25-66-01 OKAY FOR SERVICE THIS CLEARS MEL 52-16-1 MS=DDR# 131821Jun 6, 2025 · N5209A · Boeing 73783N · Escape SlideSDR SCNA20250609200Cargo Track · damagedWORK ORDER 95745, NR0004: DAMAGED TRACK ASSY CARGO SPORT IN AFT CARGO AT LBL 17.2 STA 787 - RESOLUTION: REMOVED AND REPLACED CARGO SUPPORT RAIL IN AFT CARGO AT LBL 17.2 FROM STA 727 TO STA 867 IAW B737 SRM 51-40-02.Jun 2, 2025 · N5261A · Boeing 73783N · Fuselage, Seat/Cargo Attach FittingsSDR SCNA20250602185Girt Bar · inoperativeDEFECT 813288: DOOR 1R GIRT BAR INOP - RESOLUTION: ADJUSTED GIRT BAR CLIP IAW AMM 52-00-00. GIRT BAR SECURED IN PLACE.May 31, 2025 · N831SY · Boeing 73783N · Emergency EquipmentSDR UIEA2025041200454Frame · mechanic errorFWD CARGO COMPARTMENT STA 500B LBL 21.5" FRAME I/B FLANGE WITH MIS DRILLED HOLE.(<P>REPAIRED FUSELAGE FRAME I/B FLANGE SECTION AT STA 500B BTWN STR 25LH I/A/W COOPESA COO-EO-2025-21962-R00 DATED MAR/25/2025 CATEGORY B REPAIR. DOCUMENTED ON FAA FORM 8110-3. NO Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, FrameSDR UIEA2025041400457Frame · mechanic errorFWD CARGO COMPARTMENT STA 500G LBL 21.5" FRAME I/B FLANGE WITH MIS DRILLED HOLE.(<P>REPAIRED FUSELAGE FRAME I/B FLANGE SECTION AT STA 500G BETWEEN STR 25L AND STR 27L I/A/W COOPESA COO-EO-20-25-21968- R00 REV00, DATED MAR 15-25, CATEGORY B REPAIR. DOCUMENTED Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, FrameSDR UIEA2025041400458Skin · dentedLOWER EXTERNAL FUSELAGE AT STA 893 BETWEEN STR 24R AND 25R SKIN WITH DENT.(<P>REPAIRED FUSELAGE SKIN SECTION FROM STA 887.75 TO STA 900 BETWEEN STR 23R AND 26R I/A/W COOPESA COO-EO-2025-22084-R00 REV: 00 DATED: MAR 27-25 AND BOEING MESSAGE COO-TLS-0049-03B DATApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025041400460Cargo Track · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT AT STA 500G RBL 14, TIE DOWN TRACK WITH CORROSION. NOTE: IT WAS FOUND DURING PROCESS WITH NRI 1-61.(<P>REPAIRED TIE DOWN TRACK SECTION AT RBL 13.84 FROM STA 500A + 8" TO 500G+ 19", SPLICED BETWEEN STA 500A/STA 500B AND BETWApr 22, 2025 · N5113A · Boeing 73783N · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025041400466Floorbeam · corrodedUPPER FUSELAGE MAIN CABIN, AT STA 986, BTWN RBL 50 AND LBL50, FLOOR BEAM UPPER FLANGE WITH CORROSION IN SEVERAL PLACES.(<P>REPAIRED FUSELAGE FLOOR BEAM AT STA 986.5, UPPER CHORD SECTION BETWEEN LBL 50" AND RBL 50" I/A/W COOPESA COO-EO-2025-22114-R00 REV:00, DApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor BeamSDR UIEA2025041400467Floorbeam · corrodedUPPER FUSELAGE FWD ENTRY CABIN AREA, STA 312 AT LBL1 AND LBL 8, UPPER CHORD AFT FLANGE WITH CORROSION.(<P>REPAIRED FUSELAGE FLOOR BEAM, STA 312, UPPER CHORD SECTION BETWEEN LBL 21 AND 12.25 I/A/W B-737-800 BCF SRM 53-10-51-2R-12 REPAIR 12 PARAG 1 THRU PARAG 4,Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor BeamSDR UIEA2025041400470Floorbeam · corrodedUPPER FUSELAGE FWD ENTRY CABIN AREA, STA 328 AT RBL 47 , UPPER CHORD FWD FLANGE WITH CORROSION.(<P>REPAIRED FUSELAGE FLOOR BEAM STA 328, UPPER CHORD SECTION BETWEEN RBL 32 AND RBL 64 I/A/W B-737-800 BCF SRM 53-10-21-2R-7, REPAIR 7 PARAG, FIG 204 DETAIL A SHEETApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor BeamSDR UIEA2025041400472Skin · crackedRH HORIZONTAL STABILIZER - LOWER INSPAR SKIN CRACKED AT STAB STA 101.90 (I/B SIDE OF THE RIB), 11 INCHES FWD OF THE REAR SPAR.(<P>REPAIRED R/H HORIZONTAL STABILIZER LOWER IN SPAR SKIN SECTION AT STAB STA 101.90+ 11" FWD OF THE LOWER SKIN AFT EDGE I/A/W B-737-8Apr 22, 2025 · N5113A · Boeing 73783N · Horizontal Stabilizer, Plate/SkinSDR UIEA2025041400474Cargo Track · crackedFWD CARGO COMPARTMENT AT STA 460, STA 480 RBL 13.8" CARGO TIE DOWN TRACK CRACKED AND STA 492 CORRODED AROUND ANCHOR NUT AREA. NOTE: THIS WAS FOUND WHEN PERFORMING JOB WITH NRI 1-1.(<P>REPAIRED TIE DOWN TRACK SECTION AT RBL 13.84 FROM STA 400 TO STA 500A + 16",Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025041400475Skin · crackedLEFT WING L/E SLAT #2 SKIN WITH CRACK AT ACTUATOR ATTACHEMENT FITTING LOWER SURFACE.(<P>REPAIRED L/H WING SLAT #2 (P/N:114A5020-3, S/N:001150) LEADING EDGE LOWER SURFACE SKIN SECTION AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) I/A/W B737-800 BCF SRM 57-42-01-2Apr 22, 2025 · N5113A · Boeing 73783N · Leading Edge DevicesSDR UIEA2025041600478Skin · crackedLEFT WING L/E SLAT #4 SKIN WITH CRACK AT ACTUATOR ATTACHEMENT FITTING LOWER SURFACE .<BR>(<P>REPAIRED LH WING SLAT #4 (P/N:114A5040-3, S/N:001143) LEADING EDGE LOWER SURFACE SKIN SECTION AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) I/A/W B737-800 BCF SRM 57-42-Apr 22, 2025 · N5113A · Boeing 73783N · Leading Edge DevicesSDR UIEA2025041600479Fastener · looseRH WING, SLAT N°5, IN LINE WITH HYD ACTUATOR ROD END, EXTERNAL LOWER SKIN WITH LOOSE FASTENER HEADS.(<P>REPAIRED R/H WING SLAT #5 (P/N:114A5040-4, S/N: 001120) LEADING EDGE LOWER SURFACE SKIN SECTION AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) DUE TO COUNTERSApr 22, 2025 · N5113A · Boeing 73783N · Leading Edge DevicesSDR UIEA2025041600480Fastener · looseRH WING, SLAT N°7, IN LINE WITH HYD ACTUATOR ROD END, EXTERNAL LOWER SKIN WITH LOOSE FASTENER HEADS(<P>REPAIRED R/H WING SLAT #7 (P/N:114A5020-4, S/N: 001108) WING LEADING EDGE SLAT NOSE BEAM SECTION AT THE ACTUATOR RIB AREA, PERMANENT REPAIR I/A/W B737-800 BApr 22, 2025 · N5113A · Boeing 73783N · Leading Edge DevicesSDR UIEA2025041600481Fastener · looseRH WING, SLAT N°8, IN LINE WITH HYD ACTUATOR ROD END, EXTERNAL LOWER SKIN WITH LOOSE FASTENER HEADS.(<P>REPAIRED RH WING SLAT N°8 (P/N 114A5010-4) NOSE BEAM SECTION AT ACTUATOR RIB AREA I.A.W ATLAS AIR EA-1957A223 REV 0 DATED 16-APR-25. NO FURTHER DEFECTS NOApr 22, 2025 · N5113A · Boeing 73783N · Wing Main, Frame StructureSDR UIEA2025041600482Floorbeam · crackedUPPER FUSELAGE FWD ENTRY AREA, AT STA 303.9 AND LBL 60, FLOOR ANGLE WITH CRACK.(<P>REPAIRED INNER CHORD ANGLE AT FWD ENTRY DOOR LOWER SILL, STA 303.9 WL 208, LBL 60 I/A/W COOPESA COO-EO-2025-22069-R00 REV:00 DATED: MAR-27-25, DOCUMENTED ON F.A.A FORM 8110-3. NApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Floor BeamSDR UIEA2025041600483Skin · damagedUPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 328.5 AND STR2R + 3.750", SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU (5)(6) (PROTRUDING HEApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025041600484Skin · damagedUPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 283 AND 5" BELOW STR 2R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38, REPAIR 38 PARG 4E STEP (1) THRU STEP(5) (6)(PROTRApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025041600485Skin · damagedUPPER FUSELAGE, EXTERNAL SKIN SECTION AT STA 284 AND 4.5" BELOW STR 2L SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROTApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025041600486Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 500E + 10.250" AND 2.5" BELOW STR-2L SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)Apr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025041600487Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 590 AND 1.5" ABOVE STR-3R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROTRUApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025041600488Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 649" AND 2.250" ABOVE STR-1R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) I/A/W B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP(1) THRU STEP (5)(6)( PROApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025042100553Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 819.5 AND STR-14R SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6) (PROTRUDING HEADApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025042100554Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 778.5 AND STR-1 + 2.750 INCH R, SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6) (PApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025042100555Skin · damagedUPPER FUSELAGE EXTENAL SKIN SECTION AT STA 620 AND 1 INCH BELOW STR-3L SKIN WITH LIGHTNING STRIKE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE REPAIR (REPAIR FASTENER INSTALLATION) IAW B737-800 BCF SRM 53-00-01-2R-38 REPAIR 38 PARG 4E STEP (1) THRU STEP (5)(6)( PROTRApr 22, 2025 · N5113A · Boeing 73783N · Fuselage Main, Plate/SkinSDR UIEA2025042100556Lock Fastener · looseLEFT WING, SLAT #4 LOWER L/E ACTUATOR FITTING HI-LOCKS LOOSE.(<P>REPAIRED L/H WING SLAT #4 (P/N:114A5040-3, S/N:001143) LEADING EDGE LOWER SURFACE SKIN SECTION AT THE ACTUATOR RIB AREA (PERMANENT REPAIR) IAW B373-800 BCF SRM 57-42-01-2R-8 REPAIR 8 PARG 4A THRUApr 22, 2025 · N5113A · Boeing 73783N · Leading Edge DevicesSDR UIEA2025042100557Fastener · not reportedWINGS - WING LEADING EDGE - UPPER SKIN PANEL - FASTENER CHANGE - SB 737-57-1336 R0 IAW PAR-B1920 REV.0.(<P>REPLACED FASTENER IAW ATLAS AIR PAR-B REV 0 DATED: 17JAN25 AND BOEING 737-800 BCF SRM 57-41-01-2R-7 REPAIR 7 PARG 4 TABLE 201 FIG 202, REV 23 DATED: 10MAApr 22, 2025 · N5113A · Boeing 73783N · Wing StructureSDR UIEA2025042100558Skin · crackedL/H WING, INBOARD LEADING EDGE SKIN PANEL, KRAS 206, 1 (E.A.) HOLE WITH CRACK INDICATION. CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS.(<P>PERFORMED LH WING AT KRAS 206 INBD LEADING EDGE SKIN PANEL FASTENERS OVERSIZE HOLE REPAIR IAW COO-EO-2025-2221-R00Apr 22, 2025 · N5113A · Boeing 73783N · Wing, Plate/SkinSDR UIEA2025042100559Skin · crackedR/H WING, INBOARD LEADING EDGE SKIN PANEL, KRAS 206, 1 (E.A.) HOLE WITH CRACK INDICATION. CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS.(<P>PERFORMED RH WING AT KRAS 206 INBD LEADING EDGE SKIN PANEL FASTENERS OVERSIZE HOLE REPAIR IAW COOPESA COO-EO-2025Apr 22, 2025 · N5113A · Boeing 73783N · Wing, Plate/SkinSDR SCNA20250321078Light · unsecureFLOOR LIGHTING STRIP ROW 27C LOOSE. RE-SECURED "GUIDE U" FLOOR TRACK LIGHTING STRIP AT SEAT ROW 27C REF AMM 27-51-00Mar 18, 2025 · N804SY · Boeing 73783N · Emergency LightingSDR 2025F00065Overheat Loop · faultedQRF FLIGHT 867 CCI-LPB DUE TO ENGINE #2 OVERHEAT LIGHT IS ON; FRM 261 011 52. ACCOMPLISHED FIM 26-10 TASK 810 AND THEN ENG RUNNUP NO FOUND DISCREPANCIES.Mar 15, 2025 · N317TZ · Boeing 73783N · Overheat DetectionSDR SCNA20250317076Lamp · inoperativeDEFECT 782438: RH EMERGENCY LAMP OUT. - - RESOLUTION: REMOVED AND REPLACED RH EMERGENCY LAMP IAW B737 AMM 33-51-04-960-801 OPS TEST OK AT THIS TIME.Mar 14, 2025 · N5479A · Boeing 73783N · Emergency LightingSDR SCNA20250314075Door · out of adjustWORK ORDER 93947 NR00001: TCC: INSPECT FLIGHT DECK DOOR FOR “RUBBING” ON HEADER AND POST DUE TO UNKNOWN IF DOOR IS DIFFICULT TO OPEN DUE TO DRAGGING OR SOME OTHER REASON. REFERENCE AMM 52-51-00400-801 FIG. 401 SHEET 2 FOR CLEARANCES TO HEADER AND POST. ADJUST Mar 13, 2025 · N831SY · Boeing 73783N · Fixed Inner Doors
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