Boeing 737-73V

Service difficulty reports · 1,826

Newest first. General aviation reporting is voluntary.

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 = '73773V'
  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 SWAA2022021668985Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-58310 / [01] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BFeb 4, 2022 · N7838A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2022020265510Panel · cracked193D PANEL HAS TWO FASTENER HOLE WITH CRACKS EMANATING FROM HOLES.(MARKED) / [01] REPLACED PANEL 193D; REF AMM 53-51-21; TSR 202200756Jan 29, 2022 · N558WN · Boeing 73773V · Aerodynamic FairingsSDR SWAA2022020265511Panel · cracked194E PANEL HAS TWO FASTENER HOLES WITH CRACKS EMANATING FROM HOLES. (MARKED) / [01] INSTALLED NEW PANEL IAW 53-51-21. REF TSR 202200756Jan 29, 2022 · N558WN · Boeing 73773V · Aerodynamic FairingsSDR SWAA2022021663788Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 RT SIDE AT PASSENGER CABIN (10 EA) 2022-58154 / [01] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 RT SIDE AT PASSENGER CABIJan 24, 2022 · N7838A · Boeing 73773V · Emergency LightingSDR SWAA2022021663789Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 RT SIDE AT PASSENGER CABIN (10 EA) 2022-58155 / [01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 RT SIDE AT PASSENGER CABIN (10 EJan 24, 2022 · N7838A · Boeing 73773V · Emergency LightingSDR SWAA2022021663790Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 LT SIDE AT PASSENGER CABIN (10 EA) 2022-58157 / [01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 335.25 TO STA 663 LT SIDE AT PASSENGER CABINJan 24, 2022 · N7838A · Boeing 73773V · Emergency LightingSDR SWAA2022021663791Light · missingMISSING STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 LT SIDE AT PASSENGER CABIN (10 EA) 2022-58159 / [01] INSTALLED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING END CAP BTW STA 663 TO STA 953 LT SIDE AT PASSENGER CABIN (10 Jan 24, 2022 · N7838A · Boeing 73773V · Emergency LightingSDR SWAA2022021663347Stringer · crackedCRACK STRINGER 26L LOCATED BS.540 AT FWD CARGO COMPARTMENT 2022-58135 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 03-FEB-22; TEMPERATURE CONJan 23, 2022 · N7838A · Boeing 73773V · Fuselage Main, Longeron/StringerSDR SWAA2022021663348Stringer · crackedCRACK STRINGER 27L LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58136 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 03-FEB-22; TEMPERATURE COJan 23, 2022 · N7838A · Boeing 73773V · Fuselage Main, Longeron/StringerSDR SWAA2022021663352Stringer · crackedCRACK STRINGER 27R LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58137 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] CORRECT STEP: NOMINAL THICKNESS IS: 0.056? PER NDT MANUAL 51-00-00 PART 4; PROCEDURE 3.;[03] TOOL USED THICJan 23, 2022 · N7838A · Boeing 73773V · Fuselage Main, Longeron/StringerSDR SWAA2022021663351Stringer · crackedCRACK STRINGER 25R LOCATED BS. 540 AT FWD CARGO COMPARTMENT 2022-58138 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE COJan 23, 2022 · N7838A · Boeing 73773V · Fuselage Main, Longeron/StringerSDR SWAA2022021663353Stringer · crackedCRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT 2022-58140 / [01] TOOL USED THICKNESS GAUGE PN/ 45MG; SN/ 130066701; DUE DATE/ 22-APR-2;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-22; TEMPERATURE CONTROLJan 23, 2022 · N7838A · Boeing 73773V · Fuselage Main, Longeron/StringerSDR SWAA2022021663335Panel · crackedCRACK ACCESS PANEL 194E BODY FAIRING AROUND HOLES AT LOWER FUSELAGE 2022-58095 / [01] TOOL USED CALIPER P/N 500-464 S/N 15331932 DUE DATE 26/OCT/22.;[02] TOOL USED HOTBONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22;[03] TOOL USED SCALE P/N: CL5000 S/N: AE-Jan 22, 2022 · N7838A · Boeing 73773V · Aerodynamic FairingsSDR SWAA2022021763342Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION ; 2022-58102 / REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART Jan 22, 2022 · N7838A · Boeing 73773V · Wing, Center BoxSDR SWAA2022021772410Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION 2022-58102 / [01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PAJan 22, 2022 · N7838A · Boeing 73773V · Wing, Center BoxSDR SWAA2022021872408Support Bracket · crackedCRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] REPLACED SUPPORT BRACKET (SPRING) AND FASTENERJan 21, 2022 · N7838A · Boeing 73773V · Vertical StabilizerSDR SWAA2022021663007Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 693 AT BL 0 AT PASSENGER CABIN 2022-58012 / [01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 693 AT BL 0 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 273A9110 REV. A SEE INDIVIDUAL SIGN OFFJan 21, 2022 · N7838A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2022021663008Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT BL 0 AT PASSENGER CABIN 2022-58007. REPLACED ANGLE LOC. ON FLOOR STRUCTURE BS 690 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 REV. A;[03] CORRECTED STEP 2: REPLACEJan 21, 2022 · N7838A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2022021763323Support Bracket · crackedCRACK LEADING EDGE SUPPORT BRACKET LOCATED AT BS 1016 BETWEEN S-2R AND S-2L AT VERTICAL STABILIZER ; 2022-58053 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.; [02] REPLACED SUPPORT BRACKET (SPRING) AND FASTEJan 21, 2022 · N7838A · Boeing 73773V · Vertical StabilizerSDR SWAA2022012562831Flap System · failedON APPROCH FLAPS STOPPED AT 25 NO ASSYBELLY BRAKE FLAG / [01] CHECKED FSEU FOR FAULTS NO CURRENT FAULTS NOTED PERFORMED AMM 27-51-00 AND FIM 27-51 TASK 836 AS REQ. SYSTEM OOPS CK NORMAL AT THIS TIME COULD NOT DUPLICATEJan 21, 2022 · N558WN · Boeing 73773V · Trailing Edge Flap Control SystemSDR SWAA2022012462873Seal Plate · crackedCRACK SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED THE SEAL PLATE ACCESS PANEL 333AT IAW SRM 51-10-02 ITEM 9 AND 51-40-02.Jan 20, 2022 · N7838A · Boeing 73773V · Horizontal Stabilizer, Plate/SkinSDR SWAA2022012462877Seal Plate · crackedCRACK SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED THE SEAL PLATE ACCESS PANEL 343AT IAW SRM 51-10-02 ITEM 9 AND 51-40-02.Jan 20, 2022 · N7838A · Boeing 73773V · Horizontal Stabilizer, Plate/SkinSDR SWAA2022011360711Panel · elongated193 B PANEL HAS 2 EACH OBLONG FASTERNER HOLES ON PANEL #33 AND #34 PANEL NEEDS TO BE CHANGED ; 193 B PANEL HAS 2 EACH OLONG FASTERNER HOLES ON PANEL #33 AND #34 PANEL NEEDS TO E CHANGED / [01] R&R 193 PANEL REF. SRM 51-40-02Jan 12, 2022 · N564WN · Boeing 73773V · Aerodynamic FairingsSDR SWAA2022011260724Light · inoperativeEMERGENCY EXIT LIGHTS AT L1 EXTERIOR AND R1 INTERIOR ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK AT FWD LEFT LOCATION. REF AMM 33-51-06. OP CHK GOOD.Jan 12, 2022 · N7840A · Boeing 73773V · Emergency LightingSDR SWAA2021110138234Sensor · fluctuatesON APPROACH WHEN PLACING THE FLAPS TO 15; THE LE FLAPS TRANSIT AND LE FLAPS EXT FLUCTUATED BETWEEN THE TWO LIGHTS. OVERHEAD LE DEVICES FLAPS ILLUMINATED ALL GREEN .AIRSPEED LOW AURAL AND SLOW SPEED ; RED FOOTER FLCTATED WITH ARAL WARNING. / [01] R&R LEADING EDOct 28, 2021 · N7839A · Boeing 73773V · Trailing Flap Position Indicating SystemSDR SWAA2021101228624Slide · missingCREW REPORTS FROWARD SERVICE DOOR EMERGENCY SLIDE FELL OUT ; / [01] REPACKED FS SLIDE PER MT725-61-06 AND AMM 25-66-01Oct 9, 2021 · N561WN · Boeing 73773V · Escape SlideSDR SWAA2021100827412Girt Bar · out of adjustFA REPORTS FWD SERVICE DOOR GIRT BAR HARD TO INSERT AND RELEASE ; / [01] ADJUSTED GIRT BAR TENSION AS PER SIPOct 6, 2021 · N561WN · Boeing 73773V · Escape SlideSDR SWAA2021090212712Frame · damagedREJECT- TOP FASTENER HOLE AT O/B FLANGE COMMON TO BS 500A FRAME IS ELONGATED AT FRAME REPAIR STR 7R - STR 10R ; / [01] DRILLED OVERZISE HOLE .216 FINAL SIZE AT TOP FASTENER HOLE AT O/B FLANGE COMMON TO BS 500A FRAME PER SRM 51-40-05; [02] VERIFIED CORRECTIVE AAug 28, 2021 · N7839A · Boeing 73773V · Fuselage Main, FrameSDR SWAA2021090312705Bear Strap · crackedAMOC NEEDED FOR CRACK ON THE BEAR STRAP AT THE FWD UPPER CORNER OF THE FWD GALLEY DOORWAY CUTOUT; BS 294.5 ABOVE STR 9R ; / [01] DAMAGE REPAIRED PER EA 21-153-02498 (737-700 SRM 53-10-01-2R-6; REPAIR 6). REPETITIVE INSPECTION PROGRAM DEFINED IN EA 21-153-02498Aug 26, 2021 · N7839A · Boeing 73773V · Fuselage Main, Plate/SkinSDR SWAA2021090212014Lens · missingLAV A EMERGENCY EXIT LIGHT LENS IS MISSING. / [01] REPLACED LAV A LIGHT LENS IAW AMM 33-51-01-960-802; [02] VERIFIED REPLACED LAV A LIGHT LENS IAW AMM 33-51-01-960-802Aug 25, 2021 · N7839A · Boeing 73773V · Emergency LightingSDR SWAA2021090212015Connector · not seatedLEFT OVER WING EMERGENCY EXIT LIGHT IS INOP. / [01] RESEATED CONNECTOR D11078 AT OVER WING EMERGENCY EXIT LIGHT IAW SWPM 20-61-28. PERFORMED GOOD TEST IAW AMM 33-51-00-710-801.; [02] VERIFIED CORRECTIVE ACTION #1.; [03] VERIFIED TASK IS COMPLETE.Aug 25, 2021 · N7839A · Boeing 73773V · Light System WiringSDR SWAA2021090210794Power Supply · no testEMERGENCY EXIT LIGHTS ASSOCIATED WITH M1668 ARE OUT ; / [01] UPDATED PART INFORMATION; [02] REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY M1668 AND PERFORMED GOOD TEST OF NEW POWER SUPPLY PER AMM 33-51-06-960-806.; [03] VERIFIED STEP 2; [04] VERIFIED CORRAug 23, 2021 · N7839A · Boeing 73773V · Emergency LightingSDR SWAA2021090308811Baffle · crackedFWD CARGO BAY BAFFLE IS CRACKED; BS 400-420; LBL 24; WL 154 ; / [01] LOCATED AND DRILLED (OVERSIZED ALL HOLES TO NEXT DIAMETER) NEW FWD CARGO BAY BAFFLE BS400-420; LBL 24; WL 154. PER SRM 51-40-02-0G-0 STEP 4. D. (2); BOEING DWG: 143A7505; AND SRM 51-40-05. <BAug 18, 2021 · N7839A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2021090207675Attach Angle · crackedFRAME ATTACH ANGLE AT BS 807 RBL 21 COMMON TO THRESHOLD VERTICAL WEB IS CRACKED ; / [01] REMOVED FROM FRAME ATTACH ANGLE AT BS 807 RBL 21 COMMON TO THRESHOLD VERTICAL WEB IAW SRM 51-40-02-0G-0 . PART NO HAVE ENTRIES ALLOWABLE DAMAGE IN SRM ; MUST BE REPAIRED BAug 15, 2021 · N7839A · Boeing 73773V · Fuselage Main, Attach FittingsSDR SWAA2021090307285Skin · corrodedCORROSION AROUND ADF ANTENNA MOUNTING FASTENERS HOLES. BS 694; RBL 4.8 WL 308.25. ; / [01] REMOVED CORROSION AROUND ADF ANTENNA MOUNTING FASTENERS HOLES L=1 W=1 PER REF SRM 53-00-01-1A -1 AND ARM90-7023-01; [02] VERIFIED DAMAGE REMOVED; L=32.5 W=1; PER SRM 53-Aug 14, 2021 · N7839A · Boeing 73773V · Fuselage Main, Plate/SkinSDR SWAA2021090306406Frame · damagedDAMAGE REMOVAL CUT EXTENDED INTO FRAME I/B FLANGE RADIUS AT BS 500A; STR-8R ; / [01] REPAIRED BS 500A FRAME AT STR 8 R/H IAW EA 21-153-02349; [02] COMPLETE; [03] VERIFIED COMPLETEAug 11, 2021 · N7839A · Boeing 73773V · Fuselage Main, FrameSDR SWAA2021090305896Support Angle · crackedCRACKED VERTICAL SUPPORT ANGLE ON AFT SIDE OF B.S. 663 LOWER COMPOSITE BULKHEAD AT L.B.L. 26; W.L. 150. ; / REMOVED VERTICAL SUPPORT ANGLE AFT SIDE BS 663 LOWER BULKHEAD LBL 26; WL 150 PER SRM 51-40-02; DAMAGE FOUND ON VERTICAL SUPPORT ANGLE ON AFT SIDE OF BS6Aug 10, 2021 · N7839A · Boeing 73773V · Fuselage Main, BulkheadSDR SWAA2021081605794Retainer · out of adjustFWD SERVICE GIRT BAR FALLS OUT OF CLIPS ; / [01] INSPECTED BAR CLIPS & NO DAMAGE NOTED. ADJUSTED CLIPS PER SIPAug 10, 2021 · N558WN · Boeing 73773V · Emergency EquipmentSDR SWAA2021090304845Support · crackedBAFFLE UNDER FLOOR TO SIDEWALL SUPPORT IS CRACKED; FWD CARGO BAY BS 500A-500B; RBL 24; WL 154 ; / [01] FOUND THERE TO BE NO ALLOWABLE DAMAGE FOR THIS PART THEREFOR IT IS ONLY REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-O STEP 9.; [02] REMOVED BAFFLE UNDER FLAug 7, 2021 · N7839A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2021090303915Plate · crackedRIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. ; / [01] REMOVED AND REPLACED RIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE PER AMM 53-31-31-000-802 AND AMM 53-31-31-400-802; [02] INSPECTION COMPLETEAug 4, 2021 · N7839A · Boeing 73773V · Horizontal Stabilizer StructureSDR SWAA2021090303908Panel · damagedPANEL 194 BR LOWER CENTER FASTENER HOLE ELONGATED ; PANEL 194BR LOWER CENTER FASTENER HOLE ELONGATED / DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PAR 4. REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-9 PER SRM 53-60-70-2R-1 PAR 4B(3).;Aug 4, 2021 · N7839A · Boeing 73773V · Aerodynamic FairingsSDR SWAA2021090203913Hook · corrodedRIGHT HAND EMERGENCY EXIT HATCH ESCAPE STRAP HOOK IS CORRODED. ; / [01] REMOVED AND REPLACED RIGHT HAND EMERGENCY EXIT HATCH ESCAPE STRAP. IAW AMM 25-61-10-000-802 AND AMM 25-61-10-400-802.; [02] VERIFIED REPLACEMENT OF R/H OWE HATCH ESCAPE STRAP PER AMM 25-61Aug 4, 2021 · N7839A · Boeing 73773V · Emergency EquipmentSDR SWAA2021090203914Strap · corrodedLEFT HAND EMERGENCY EXIT HATCH ESCAPE STRAP HOOK IS CORRODED. ; / [01] REMOVED AND REPLACED LEFT HAND EMERGENCY EXIT HATCH ESCAPE STRAP. IAW AMM 25-61-10-000-802 AND AMM 25-61-10-400-802; [02] VERIFIED REPLACEMENT OF L/H OWE HATCH ESCAPE STRAP PER AMM 25-61-10Aug 4, 2021 · N7839A · Boeing 73773V · Emergency EquipmentSDR SWAA2021090203917Stringer Clip · chafedP18 PANEL ATTACH CLIP IS CHAFED AT STRINGER 6 LEFT; B.S. 262. ; / [01] REMOVED CLIP LOCATED AT BS. 262 STR6L IAW 51-40-02 AND SRM 51-20-02 ITEM 9.C MUST BE REPAIRED BY REPLACEMENT NO ENTRIES EN SRM .; [02] FABRICATED CLIP FROM MATERIAL 6013T4. BARE 0.050' LOT.Aug 4, 2021 · N7839A · Boeing 73773V · Fuselage Main, Attach FittingsSDR SWAA2021080903912Hook · corrodedLEFT HAND EMERGENCY EXIT HATCH ESCAPE STRAP HOOK IS CORRODED. ; / [01] FAULT WILL BE RESOLVED ON FAULT TTG8Q0061VHR.; [02] VERIFIED FAULT WILL BE RESOLVED ON FAULT TTG8Q0061VHR.Aug 4, 2021 · N7839A · Boeing 73773V · Emergency EquipmentSDR SWAA2021090303506Support · crackedCRACKED INTERCOSTAL AT AFT PASSENGER CABIN BS943 BL0 WL208. ; / [01] REMOVED INTERCOSTAL AY BS 943 BL 0 WL 208 PER SRM 51-40-02-GO-0; [02] EVALUATED CRACK ON INTERCOSTAL AT AFT PASSENGER CABIN BS 943 BL0 WL208 AND FOUND OUT OF LIMITS IAW SRM 53-70-51-1A-1 PAR.Aug 3, 2021 · N7839A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2021090303503Channel · corrodedCORROSION ON MOP SILL AT AFT PASSENGER CABIN BS951-BS991 LBL49 WL208. ; / REMOVED CORROSION ON AFT PASSENGER CABIN MOP SILL BS 951 - BS 991 LBL 49 WL 208 MAX. MAT. LOSS 6' X 3' X .012' ORIGINAL THICKNESS .080' FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-70-15-1A-]Aug 3, 2021 · N7839A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2021090303502Strap · corrodedCORROSION ON TENSION STRAP AT AFT PASSENGER CABIN BS1026 RBL3 WL208. ; / [01] VERIFIED NO ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH 9C.; [02] CORRECTED MEASUREMENT; [03] VERIFIED CORRECAug 3, 2021 · N7839A · Boeing 73773V · Fuselage Miscellaneous StructureSDR SWAA2021090303494Support · damagedPNEUMATIC DUCT CLAMP SUPPORT HAS ELONGATED MOUNT HOLE AT INBOARD FRONT SPAR STATION 151 ON LEFT WING INBOARD FRONT SPAR. ; / [01] REMOVED AND REPLACED PNEUMATIC DUCT CLAMP SUPPORT AT INBOARD FRONT SPAR STA.151 ON LEFT WING INBOARD SPAR IAW: <BR>AMM 36-13-01-00Aug 3, 2021 · N7839A · Boeing 73773V · Wing Miscellaneous StructureSDR SWAA2021090203507Support · crackedCRACKED INTERCOSTAL AT FWD WET AREA BS317 RBL31 WL208. ; / [01] VERIFIED APPLICABILITY OF SRM 53-10-51-0I-2 FOR IDENTIFICATION AND NO FOUND ALLOWABLE DAMAGE FOR THIS PART. REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; PAR.9.C.; [02] VERIFIED APPLICABILITY OAug 3, 2021 · N7839A · Boeing 73773V · Fuselage Miscellaneous Structure
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