Boeing 737-76Q
Service difficulty reports · 1,627
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 = '73776Q' 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.
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 = '73776Q' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2023053128262Stringer · corrodedCORROSION STRINGER 26L LOCATED BS540 AND WL156 AT FWD CARGO COMPARTMENT 2023-258027<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 221860711 AND DUE DATE: 07-NOV-23.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-SDR SWAA2023053128261Stringer · corrodedCORROSION STRINGER 27R LOCATED BS540 AND WL150 AT FWD CARGO COMPARTMENT 2023-258025<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 221860711 AND DUE DATE: 07-NOV-23.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-SDR SWAA2023053128270Stringer · corrodedCORROSION STRINGER 23L LOCATED BS540 AND WL164 AT FWD CARGO COMPARTMENT 2023-258028<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 221860711 AND DUE DATE: 07-NOV-23.;[02] TOOL USED EDDY FLAW DETECTOR P/N: NORTEC 600D; S/N: 210138003; DUE DATA: 27-MAR-24.;[03] SDR SWAA2023050928225Panel · pulledPANEL 661BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4B( REPAIRED PER SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PARA 4C AND TABLE 202. <BR><BR>REMOVED DAMAGE TO ALL FASTENER HOLES OSDR SWAA2023050928226Panel · pulledPANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED) FOUND PANEL TO BE 661AB. PANEL 561AB FASTENER HOLES WILL BE REPAIRED ON FAULT TTG8Q00KCULF<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4B(5).REPAIRED PER SRM 51-70-04-2R-9 AS DIRECTSDR SWAA2023053128081Stringer · corrodedCORROSION STRINGER 23R LOCATED BS500B PLUS 5INCH AT FWD CARGO COMPARTMENT 2023-257972<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN:45MG; SN:130064101; DUE DATE: 12-OCT-23;[02] TOOL USED: ULTRASONIC THICKNESS EQUIPMENT; P/N: 45 MG; S/N: 130066401; DUE DATE: 2SDR SWAA2023053128082Stringer · corrodedCORROSION STRINGER 23L LOCATED BS500B PLUS 5INCH AT FWD CARGO COMPARTMENT 2023-257973<[01] TOOL USED EDDY FLAW DETECTOR P/N: NORTEC 600D; S/N: 210138003; DUE DATA: 27-MAR-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATESDR SWAA2023053128077Angle · crackedCRACK ANGLE LOCATED BS500C FWD FACE AT LEVEL STR26R FWD CARGO COMPARTMENT 2023-257978<[01] REPLACED ANGLE LOCATED BS500C FWD FACE AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING #143A7505 REV: D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] SDR SWAA2023053128084Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2023-257976<[01] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG 143A7902 SHEET 174 REV -;[02] CORRECTED STEP 1.<BR>REPLACED GUSSET LSDR SWAA2023053128085Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-257977<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DWG 143A7902 SHEET 174 REV -;[02] CORRECTED STEP 1.<BR>REPLACED GUSSET LOCASDR SWAA2023053127996Support Angle · crackedCRACK SUPPORT ANGLE BS 695 AND BL 0 CENTER SECTION 2023-257932<[01] REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL 0 CENTER SECTION AND FASTENERS IAW B737-700 SRM 51-40-05 AND DWG: 273A9110 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED SDR SWAA2023053128086Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 184.70 RIB AND 8 INCH. FROM REAR SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.400 INCH. APPROX. 2023-257980<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 21SDR SWAA2023053127997Bracket · crackedCRACK BRACKET ASSY BS 540 BTW BL0 TO LBL 24.75 AT PASSENGER CABIN 2023-257937<[01] REPLACED BRACKET ASSY BS 540 BTW BL0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED BRACKET ASSY SDR SWAA2023053127998Bracket · crackedCRACK BRACKET ASSY BS 540 BTW BL0 TO RBL 24.75 AT PASSENGER CABIN 2023-257940<[01] REPLACED BRACKET ASSY BS 540 BTW BL0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED BRACKET ASSY SDR SWAA2023050927775Skin · debondedPANEL 191FR OUTER SKIN IS DISBONDED. (MARKED)<[01] IDENTIFIED PANEL 191FR IAW SRM 53-30-70-0I-1; FIGURE 2; SHEET 1; TABLE 2; ITEM 4.<BR><BR>CLEANED PANEL FOR EVALUATION IAW AMM 51-21-11-150-815 PARA 17. C.<BR><BR>VISUALLY EXAMINED DAMAGE AND TAP TESTED WITH DISDR SWAA2023050827777Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 4. DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1508290-1 USING BMS5-107 LOT AK2KP8383K-1 RESIN WISDR SWAA2023050827778Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241AF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR PSDR SWAA2023050827779Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241BF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR PSDR SWAA2023050827780Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-17 LOT 1522265-1 USING BMS5-107 LOT AK2KP8383K-1 RESIN WITH THE INSERTS; CURED THE RESIN UNDER A HEAT LAMP USING TSDR SWAA2023050827781Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 UNDER SEAT LOW TRAFFIC SECTION 44.<BR>MULTIPLE PULLED STRANDS; DENTS & OTHER DEFECTS EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-0SDR SWAA2023050827782Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 4; TABLE 4.<BR><BR>UPON INVESTIGATION; PANEL DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM<BR>53-00-50-1A-1 PAR. 4. E. & 4. F.<BR><BSDR SWAA2023050827784Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 232SF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. FLOOR PANEL IS DAMAGED BEYOND ECONOMICAL REPAIR; AND EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLOOR SDR SWAA2023053127377Scuff Plate · crackedCRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-257912<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21143424;DUE DATE:03-NOV-23.;[02] RADIOMETER PHOTOMETER P/N XRP-3000 S/N 1859843 DUE DATE 04-MAY-23.;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFSDR SWAA2023053127376Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-257910<[01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A16165044; DUE DATE 12-MAR-24.;[02] RADIOMETER PHOTOMETER P/N XRP-3000 S/N 1859843 DUE DATE 04-MAY-23.;[03] REPAIRED FWD CORNER SCUFF PLATE SDR SWAA2023053127586Panel · crackedCRACK ACCESS PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR 2023-257914<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:26-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18196126 DUE DATE: 26-MAR-24.;[03] TOOL USED: SACLE P/N: SPX621 S/N:SDR SWAA2023053127587Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2023-257916<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189416; DUE DATE: 19-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9000B-AV; S/N: 18185761; DUE DATE: 24-SEP-23.;[03] TOOL USED: SCALE P/N: CR52SDR SWAA2023050927757Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT ACB BS827 LBL6 WL157.<[01] FOUND TO BE WITH NO LIMITS PER SRM 53-00-53-1A2;[02] REMOVED STRINGER CLIP IAW SRM 51-40-02;[03] RECEIVED NEW STRINGER CLIP LOCATED AND DRILLED<BR>AT ACB BS827 LBL6 WL 157<BR>P/N 146A1010-10 LOT# 1478113SDR SWAA2023050927747Support · corrodedCORROSION ON FLOOR SUPPORT SPLICE AT ACB BS727D+6 LBL20 TO RBL20 WL156.<[01] THIS PART DOES NOT ALLOWABLE DAMAGE LIMITS; IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RECEIVED NEW SPLICE STRIP ASSY ATSDR SWAA2023050927769Stringer · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED<[01] CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT ALLOWED IAW SRM 53-00-03-1A-1 .<BR>CUT AND REMOVED THE DAMAGED PART OF SDR SWAA2023050927768Stringer · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-27R WL150. MARKED<[01] CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-267R WL150 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT ALLOWED IAW SRM 53-00-03-1A-1 .<BR>CUT AND REMOVED THE DAMAGED PART OFSDR SWAA2023050927755Intercostal · corrodedCORROSION ON INTERCOASTAL AT ACB BS847+9 RBL6 WL159.<[01] VERIFY APPLICABILITY PER SRM53-60-15-0I-1 AND SRM 53-60-15-1A-1<BR>REMOVED CORROSION AT DISCREPANCY AREA L=3'; W=1.5' PER SRM 51-10-02-0G-0 AND SRM 53-60-15-1A-1;[02] VERIFIED CORRECTIVE ACTION 1.;[03] SDR SWAA2023050927748Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB LBL21 BS727A - BS807 WL156.<[01] SRM 53-60-53-0I-2 IDENTIFICATION AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 ARE APPLICABLE;[02] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT UPPER SURFACE 03 EACH LOCATIONS L=19' ; SDR SWAA2023050927751Attach Angle · corrodedCORROSION ON INTERCOSTAL TO WEB ATTACH ANGLE BS767+2; 767+5; 767+9; 767+16; 767+19 RBL21 WL156.<[01] FOUND TO BE OUT OF LIMITS EXFOLIATED CORRODED WITH MORE THE 50 % OF MATERIAL LOST IWA B 737-700 SRM 53-60-15 REMOVED DAMAGE PART PER SRM 51-40-02;[02] SRM 53-6SDR SWAA2023050927749Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB RBL21 BS727B+4; BS727C+14 - BS767 WL156.<[01] VERIFY APPLICABILITY PER SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2.<BR>REMOVED CORROSION ON DISCREPANCY AREA L=0.800';W=0.700';D=0.010'. FOUND TO BE OUT OF LIMITS IAW SRMSDR SWAA2023050927764Shield · corrodedCORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 RBL24 WL156.<[01] AFT SHIELD AT FORWARD CARGO BAY LOCATED BETWEEN BS492.4- BS500A RBL 24 WL 156 NOT HAS ENTRIES ALLOWABLE DAMAGE IN SRM. MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAGRAPH 9.C.;[02] VERIFIED SDR SWAA2023050927750Cargo Track · corrodedCORROSION ON TRACK AT ACB BS787+12 RBL14 WL157.<FOUND TO OUT OF LIMITS ORIGINAL MATERIAL .070 REMAINING MATERIAL .060 ALLOWABLE DAMAGE LIMITS IS .007.;[13] UPDATED CORRECTIVE ACTION 5. REMOVED NUTPLATE PER B737-700 SRM 51-40-02-0G-0.;[14] OBTAINED LOCATED AND SDR SWAA2023050927762Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS500D LBL23 WL156.<OUT OF LIMITS; WILL BE REPAIR BY REPLACEMENT PER SRM 51-10-02 PARAG. 9.C;[05] RECEIVED EXTRUSION P/N BAC1496-444 LOT. 1524635-1. LOCATED AND DRILLED (2EA) EXTRUSION (FORMED CHANNEL) ON FSDR SWAA2023050927767Intercostal · crackedCRACKED INTERCOSTAL AT AREA AFT OF FCB BS500D+18 RBL31 S-25R WL159.<[01] REMOVED INTERCOSTAL AT AREA AFT OF FCB BS500D+18 RBL31 S-25R WL159 IAW SRM 51-40-02.-;[02] RECEIVED NEW INTERCOSTAL HFAB53-AN-011 (7075T0#0.032'') PER DWG# 143A9803-58 HEAT TREATED TO T62SDR SWAA2023050927758Attach Angle · corrodedCORROSION ON ATTACH ANGLE AT ACB BS727E LBL7 WL152.<[01] FOUND TO BE WITH NO LIMITS IAW SRM 53-00-53-1A-2;[02] PART TO BE REPAIR BY REPLACEMENT PEER SRM 51-10-02 PARAGRAPH 9.C;[03] REMOVED ATTACH ANGLE AT ACB BS 727E LBL7 WL 152 IAW SRM 51-40-02;[04] RECEIVED SDR SWAA2023050827765Attach Angle · crackedFWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500A FWD SIDE LBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER SSDR SWAA2023050827766Attach Angle · crackedFWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500B FWD SIDE RBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL;FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER SSDR SWAA2023053127369Fitting · wornWEAR ON GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2023-257904<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801 STEP 3. D (1) (I);[02] REPLACED GIRT BAR FITTING HARDSDR SWAA2023053126858Lens · crackedCRACK EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA 2023-257865<[01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802 STEP C (5) (D) AND C (10).;[02] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B ATSDR SWAA2023053126853Light · crackedCRACK GALLEY 4 EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA 2023-257859<[01] REPLACED GALLEY 4 EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802.TEST IS OK.;[02] REPLACED GALLEY 4 EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA I.A.SDR SWAA2023053127372Fitting · wornWEAR ON GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT AFT GALLEY AREA 2023-257907<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT ATF GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801 STEP 3. D (1) (I);[02] REPLACED GIRT BAR FITTING HARDSDR SWAA2023053127370Support Bracket · crackedCRACK SUPPORT BRACKET AIR DUCT BS 540 AND RBL 7 AT AIR CONDITIONING BAY 2023-257901<[01] FAULT RESOLVED ON OTHER FAULT .SEE TTG8Q00KU567;[02] JOB COMPLETEDSDR SWAA2023053127171Bracket · crackedCRACK BRACKET BODY STATION 552 AND LBL 6 KEEL BEAM 2023-257887<[01] REPLACED BRACKET BODY STATION 552 AND LBL 6 KEEL BEAM I.A.W B737-700 SRM 51-40-02 AND DWG# 149A7701; SHEET 2; REV.A.;[02] COMPLETEDSDR SWAA2023053127172Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 578 AND LBL 6 KEEL BEAM 2023-257888<[01] REPLACED SUPPORT BRACKET BODY STATION 578 AND LBL 6 KEEL BEAM I.A.W B737-700 SRM 51-40-02 AND DWG# 149A7701; SHEET 2; REV.A.;[02] CERTIFIED STEP 1 COMPLETEDSDR SWAA2023053127371Angle · crackedCRACK INTERNAL AREA RT SIDE BODY STA 663.75 SUPPORT ANGLE AT AIR CONDITIONING BAY 2023-257905<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 14SDR SWAA2023050827319Frame · crackedCRACK ON PASSENGER CABIN FRAME AT BS 727B STRINGER BETWEEN 8L-9L.(MARKED)<[01] FORMED ANGLE REPAIR PART B PER EA 1-A53-12114 APPENDIX REV A OK TO HEAT AND TRAET;[02] MATERIAL ID 7075-0 .050 LOT # 1517365-2;[03] REMOVED DAMAGE PER EA 1-A53-12114;[04] WORK ACCOM
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