Boeing 737-752

Service difficulty reports · 2,590

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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 = '737752'
  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 SWAA2021101320675Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 870 RBL 22, WL166. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED, FABRICATED LOCATED, AND A DRILLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0, AND DWG 146ASep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101319797None · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL21 WL164. CORROSION ON ACB AFT SHIELD AT BS847 - BS867 ; RBL21 WL164 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM FOR THIS ITEM IAW SRM 51-10-02-0G-0.Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101319798Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 807 - 727C, LBL 21 WL 156. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2.Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101319780Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767 - BS727B RBL21 WL156. ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS727B - BS767 RBL 21 WL 156 ; ORIGINAL THICKNESS IS 0.040' ; MAXIMUM MATERIAL REMOVED IS 1'X1.5'X0.011' ; REMAINSep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101319779Strap · corrodedCORROSION ON STRAP IN AFT CARGO BAY BS 809, RBL 19, WL 159. REMOVED CORROSION ON STRAP IAW SRM 51-10-02-0G-0 MEASURE L=1.6'X W=1.4'X D=0.025' MAX. MAT LOSS IS 0.025'. REMAINING THICKNESS IS 0.055'; ORIGINAL THICKNESS IS 0.080' FOUND TO BE OUT OF LIMITS. RSep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101320678Strap · corrodedCORROSION ON STRAP AT AFT CARGO BAY BS809 RBL19 WL159. ; / [04] RECIVED NEW STRAP ITEM 146A8128U14 LOT 1468918 LOCATED AND DRILLED NEW STRAP AT BS 809 RBL19 WL159; IAW B 737-700 SRM 51-40-05-OG-0 DWG 146A8128 OK TO INSTALL.-; [05] VERIFIED CORRECTIVE ACTION 4;Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220674Support Splice · corrodedCORROSION ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 LBL8 TO RBL13 WL168. FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW SPLICE IAW SRM 51-40-05-OG-0, AND DWG 146A9401. REMOVED AND INSTALLED SPLICE STRAP TO BE INSTALLED ON TTG8Q004C7C0.Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220696Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS 847 - 867, RBL 21, WL 164. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. LOCATED AND DRILLED A NEW AFT SHIELD IAW SRM 51-40-05, AND DWG 146A0081. INSTALLED THE NEW SHIELD BETWEEN BS 847 - 867, RBL 21, WL 164Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220679Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767 - BS727B RBL21 WL156. ; / [12] REMOVED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727- BS 747 RBL21 WL156 IAW SRM 51-40-02-0G-0; [13] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT BS 727-BS747 RBSep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220694Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS899 RBL22 WL170. ; / [11] INSTALLED SPLICE ON FLOOR TO SIDEWALL SUPPORT OF AFT CARGO BAY AT BS887 RBL22 WL170. I.A.W. DWG# 146A7502; SRM 51-40-02.; [12] VERIFIED CORRECTIVE ACTION 11.; [13] OK TO INTALLSep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101219776Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS870 RBL22 WL166. ; / [11] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT BS 867-BS887 RBL22 WL166 . IAW 773-700 SRM 51-40-02-0G-0; DWG 146A7500. ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINSep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101219783Shield · corrodedCORROSION ON FWD SHIELD AT AFT CARGO BAY BS 767 - 787, RBL22 WL157. FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW ACB FWD SHIELD IAW SRM 51-40-05 AND DWG 146A0081. INSTALLED ACB FWD SHIELD IAW SRM 51-40-02-0G-0, AND DGW 146A0081.Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220707Cargo Track · corrodedCORROSION ON CARGO TRACK, AFT CARGO BAY BS 727E+9, LBL 3, WL 156. REMOVED CORROSION, AND FOUND OUT OF LIMITS. IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, STEP 4(2). DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q006LBGL.Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021101220704Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS792 RBL19 WL158. RECIVED NEW WEB ITEM HFAB53-WB-011. LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-OG-0 DWG 146A8123 . APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW AMM 51-21-72-370-804, & AMM 51-21-41-370-802. INSTASep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220701Strap · corrodedCORROSION ON STRAP IN THE AFT CARGO BAY, BS 797, RBL 19, WL 158. REMOVED CORROSION ON STRAP IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS. REWORKED AREA IAW SRM53-60-15-1A-1, ALLOWABLE DAMAGE PARAG. 4.G (3) DETAIL (B) FIG 103. STRAP WILL BE REPLACED Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220697Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT IN THE AFT CARGO BAY, BS 807 - 727C, LBL 21, WL 156. FABRICATED, LOCATED, AND DRILLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0, AND DWG 146A7500, FABRICATED LOCATE AND DRILLED A DOUBLER IAW SRM 53-00-53-2R-Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220692Attach Angle · corrodedCORROSION ON ATTACH ANGLE AT THE AFT CARGO BAY BS 727C, RBL 7, WL 151. REMOVED ATTACH ANGLE IAW SRM 51-40-02-0G-0. FABRICATED A NEW ATTACH ANGLE. LOCATED, AND DRILL IAW SRM 51-40-05 AND DWG 146A1320. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW AMM 5Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Main, Attach FittingsSDR SWAA2021101220691Attach Angle · corrodedCORROSION ON ATTACH ANGLE BS 727D, RBL 7, WL 151. REMOVED ATTACH ANGLE IAW SRM 51-40-02-0G-0. FABRICATED A NEW ATTACH ANGLE. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A1320. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW AMM 51-21-41-370-802, ASep 18, 2021 · N7843A · Boeing 737752 · Fuselage Main, Attach FittingsSDR SWAA2021101220690Attach Angle · corrodedCORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D RBL6 WL151. REMOVED ATTACH ANGLE IAW SRM 51-40-02-0G-0. FABRICATED A NEW ATTACH ANGLE. LOCATED AND DRILL IAW SRM 51-40-05 AND DWG#146A1320. INSTALLED ATTACH ANGLE IAW SRM 51-40-02 PAR 7, DWG 146A7500, ANSep 18, 2021 · N7843A · Boeing 737752 · Fuselage Main, Attach FittingsSDR SWAA2021101220689Cargo Track · corrodedCORROSION ON RAIL AT AFT CARGO BAY BS727D+12 LBL3 WL156. ; / ; [15] INSTALLED REPAIR PARTS AT AFT CARGO BAY BETWEEN BS 727C + 13' TO BS 727E + 10' LBL 3 WL 156 PER SRM 53-00-53-2R-2 REP. 2 ALTERNATIVE 1 FIG. 204 AND ALTERNATIVE 5 FIG. 208 STEP 4 P;Q AND R; [16Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021101220683Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS775 RBL19 WL157. LOCATED AND DRILLED A NEW WEB IAW SRM 51-40-05-OG-0 DWG 146A8123. REMOVED THE WEB IAW SRM 51-40-02. INSTALLED THE INTERCOSTAL WEB IAW SRM 51-40-02 AND IAW DWG 146A0081.Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220681Strap · corrodedCORROSION ON STRAP AT AFT CARGO BAY BS789 RBL19 WL158. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS. REWORKED AREA IAW SRM 53-60-15-1A-1, ALLOWABLE DAMAGE PARAG. 4.G (3) DETAIL (B) FIG 103. STRAP REPLACED ON CARD TTG8Q006LB76.Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220680Strap · corrodedCORROSION ON STRAP IN THE AFT CARGO BAY BS 794, RBL 19, WL 158. REMOVED CORROSION IAW SRM 51-10-02-0G-0 MEASURE L=1.5'X W=1.4'X D=0.015' MAX. MAT LOSS IS 0.015'; REMAINING THICKNESS IS 0.065'; ORIGINAL THICKNESS IS 0.080' FOUND TO BE OUT OF LIMITS. REWORSep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101220676None · corrodedCORROSION ON SUBTHRESHOLD WEB, AFT CARGO BAY BS 795 - 847, RBL 26, WL 160. REMOVED CORROSION &FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 PARAG.4.G.(2) DETAIL G FIG.103. REMOVED SUBTHRESHOLD WEB IAW SRM 51-40-02. LOCATED &DRILLED THESep 18, 2021 · N7843A · Boeing 737752 · Fuselage Main, StructureSDR SWAA2021101220673Support · corrodedCORROSION ON AFT BULKHEAD TO SIDEWALL SUPPORT AT AFT CARGO BAY BS947 RBL22 WL181. ; / [10] INSTALLED NEW AFT BULKHEAD TO SIDEWALL SUPPORT AT AFT CARGO BAY BS947 RBL22 WL181; ITEM 149A8118-28; LOT#1469760; IAW SRM 51-40-02-0G-0 AND DWG#149A8117 AND DWG#147A0020Sep 18, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101319773Scuff Plate · crackedFWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED CRACKED RADIUS OF FCB AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, PARA 4. B. (2) AND (4). FLUORESCENT DYE PENETRANT INSPECTED ON REPAIRED AREA IAW SOPM 20-20-02 METHOD C. NO DEFECTS NOTED. SANDED Sep 17, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101320672Scuff Plate · crackedFWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. WELDED CRACKED RADIUS OF FCB, AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1 PARA 4. B. (2) AND (4). FLUORESCENT DYE PENETRANT INSPECTED OF REPAIRED AREA IAW SOPM 20-20-02 METHOD C. NO DEFECTS NOTED SANDED REPAISep 17, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101319769Panel · crackedPANEL 191FL HAS SEVERAL CRACKED / PULLED THROUGH FASTENER ATTACH HOLES ; / [01] PART/MATERIAL IDENTIFIED PER SRM 53-30-70-0I-1 FIG 2 TABLE 2 ITEM 4 .<BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE AS GIVEN IN SRM 53-30-70-1A-1 PARA 4 B .<BR>REPAIR TO BE PERFORMED IAW SRM Sep 17, 2021 · N7843A · Boeing 737752 · Fuselage Floor PanelSDR SWAA2021101320669Floor Panel · crackedPANEL 191FR HAS SEVERAL CRACKED & PULLED THROUGH FASTENER HOLES. EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-70-1A-1 PARAGRAPH 4.B(6). REMOVED DAMAGE AND UPSIZED HOLES. PREPPED AND CLEANED HOLES IAW SRM 51-70-04-2R-9 PARAGRAPH 4.A-C. APPLIED FIBERGLASS/RSep 17, 2021 · N7843A · Boeing 737752 · Fuselage Floor PanelSDR SWAA2021101320667Web · corrodedCRACKED SUPPORT BRACKET BTW ORSS 261 TO ORSS 297 LT WING. REMOVED SUPPORT BRACKET NO ALLOWABLE DAMAGE LIMITS FOR CRACK IAW SRM 51-40-02. MEASURE OF CRACK IS 0.614. DRILLED NEW SUPPORT BRACKET IAW SRM 51-40-05. APPLIED PROTECTIVE TREATMENT ON ALL OPEN Sep 16, 2021 · N7843A · Boeing 737752 · Fuselage Main, StructureSDR SWAA2021101319762Intercostal · corrodedSUPPORT INTERCOSTAL IS CORRODED ON UPPER SURFACE AT BS 259 - 270, WL 207.54, LBL 3 - RBL 3. REMOVED DAMAGE ON INTERCOSTAL IAW SRM 51-10-02-0G-0. ORIGINAL MATERIAL THICKNESS .040' IAW SRM 53-10-51-0I-2, REMAINING MAT. THICKNESS .030' FOUND TO BE OUT OF LIMITSSep 16, 2021 · N7843A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021101318316Floorbeam · crackedCRACKED FLOORBEAM, BS 540, BL 0 - LBL 24.5, WL 208.1. REMOVED FLOORBEAM IAW SRM 51-40-02-0G-0. LOCATED & DRILLED NEW FLOORBEAM IAW SRM 51-40-05-0G-0, AND DWG 143A0060, SHEET 46. INSTALLED THE NEW FLOORBEAM IAW SRM 51-40-02-0G-0, AND DWG 143A0060.Sep 15, 2021 · N7843A · Boeing 737752 · Fuselage Main, Floor BeamSDR SWAA2021101318281Seal Plate · crackedLEFT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. REMOVED AND REPLACED THE LT HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802.Sep 14, 2021 · N7843A · Boeing 737752 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2021101318287Seal Plate · crackedRIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. 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.Sep 14, 2021 · N7843A · Boeing 737752 · Horizontal Stabilizer StructureSDR SWAA2021101318263Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED. REMOVED CRACK DAMAGE AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4.Sep 14, 2021 · N7843A · Boeing 737752 · Horizontal Stabilizer StructureSDR SWAA2021101317030None · crackedCRACK AROUND THE FASTENER AT NR 8 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. FABRICATED REPAIR AND FILLER, APPLIED CHEMICAL CONVERSION COATING IAW SRM 57-42-01-2R-8. APPLIED PRIMER TO REPAIR AND INSTALLED COUNTERSINK REPAIR WASHERS IAW Sep 11, 2021 · N7843A · Boeing 737752 · Leading Edge DevicesSDR SWAA2021101317029None · crackedCRACK AROUND THE FASTENER AT NO.3 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN. INSTALLED REPAIR IAW SRM 57-42-01-2R-8. STEP 4L. AND 21-157-02763-WIP1. INSTALLED ACCESS PANELS AND FLEX SKIN IAW SRM 51-40-02.Sep 11, 2021 · N7843A · Boeing 737752 · Leading Edge DevicesSDR SWAA2021090713813Processor · inoperativeCENTER TANK FUEL QUANTITY INDICATION INOP IN CRUISE. ; / [01] OK TO CONTINUE PER MEL 28-7-01. SP1; SP3; SP28; [02] REMOVED AND REPLACED FUEL QUANTITY PROCESSOR UNIT PER AMM 28-41-81. OPS CHECK GOOD. THIS CLEARS MEL 28-7-01. REF LOGPAGE# 1825844.Aug 31, 2021 · N7887A · Boeing 737752 · Fuel Quantity IndicatorSDR SWAA2021081104846Radome · delaminatedINSPECTED RADOME ON NOSE AND FOUND CIRCULAR DE-LAMINATIONS. DECAY AND DAMAGE TO NOSE RADOME AND DETERIORATION OF THE NOSE RADOME SURFACE. ; / [01] REMOVED AND REPLACED NOSE RADOME IAW AMM 53-52-00.Aug 7, 2021 · N7843A · Boeing 737752 · Aerodynamic FairingsSDR SWAA2021071393693Line · damagedPACKS UNABLE TO MAINTAIN CABIN PRESSURISATION WITH IDLE THRUST @ FL280 ALTITUDE WARNING ; / [01] TROUBLESHOT & FOUND DAMAGED SENSE LINE FROM 9TH STAGE DUCT; CONNECTING TO HIGHSTAGE REGULATOR. REF SOPM 20-50-00. PERFORMED PACK CONFIDENCE CHECK MT 721-00-01 & EXJul 9, 2021 · N7847A · Boeing 737752 · Cabin Pressure Control SystemSDR SWAA2021070890623Light · inoperativeEXTERIOR ESCAPE SLIDE LIGHT AFT OF DOOR 2L INOP ; / [01] REVAMPED EMERGENCY ESCAPE SLIDE LIGHT AFT OF DOOR 2L REF AMM 33-51-04. OPS CHECK NORMAL.Jul 4, 2021 · N7847A · Boeing 737752 · Emergency LightingSDR SWAA2021072690621Rib · crackedCRACK INSPAR RIB STAB ST 120.30 AT 19 INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-296644 / [01] EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101U102020 DUE DATE: 01-JUN-22.; [02] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101U10Jul 1, 2021 · N7844A · Boeing 737752 · Horizontal Stabilizer, Spar/RibSDR SWAA2021072689360Support Angle · crackedCRACK ANGLE - SUPPORT LOC ON BS 791 APPROX AT LEVEL OF STR 18R AFT CARGO COMPARTMENT ; 2021-296595 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22.; [02] REPLACED ANGLE SUPPORT LOC ON BS 791 APPROX AT LEVEL OF Jun 29, 2021 · N7844A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021072688647Angle · crackedCRACK ANGLE GUSSET LOCATED ON BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT ; 2021-296556 / [01] REPLACED ANGLE GUSSET AND FASTENERS LOCATED ON BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 STEP 9 AND DRAWING # 14Jun 27, 2021 · N7844A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021072688648Angle · crackedCRACK ANGLE GUSSET LOCATED ON BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT ; 2021-296558 / [01] REPLACED ANGLE GUSSET LOCATED ON BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9 AND DWG 143A7902 REV -; [0Jun 27, 2021 · N7844A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2021072688276Skin · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STA 193.90 AND 16 INCH. FROM THE FRONT SPAR. LENGTH = 0.900 INCH. APPROX. ; 2021-296464 / [01] TOOL USED: P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 24-FEB-22; [02] TOOL USED CALIPER PN:Jun 27, 2021 · N7844A · Boeing 737752 · Horizontal Stabilizer, Plate/SkinSDR SWAA2021072688270Retainer · crackedCRACK ACCESS PANEL 643BB SEAL RETAINER AT RT WING ; 2021-296444 / [01] REPLACED SEAL RETAINER LOCATED PANEL 643BB AT RT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0. CRACK LENGTH: 1.000 TOOL USED DIGITAL CALIPER: P/N:700-113-10 S/N:0016656 Jun 26, 2021 · N7844A · Boeing 737752 · Wing Main, Frame StructureSDR SWAA2021072690620Skin · dentedDENT EXTERNAL SKIN LOC AT BS 360 MORE 12 INCH AT STR 19 L AT LOWER FUSELAGE ; 2021-296403 / [01] TOOL USED P/N: NORTEC 600D; S/N2000053402; DUE DATE: 23-APR-22; [02] TOOL USED CALIPER P/N: DIGITAL 150 ; S/N: AE-412604 DUE DATE: 28-MAY-22 AND DENT GAUGE P/N:PGKJun 26, 2021 · N7844A · Boeing 737752 · Fuselage Main, Plate/SkinSDR SWAA2021072688260Rib · crackedCRACK LEADING EDGE RIB STAB ST 198.23 AT RT HORIZONTAL STABILIZER ; 2021-296386 / [01] REPLACED RIB LEADING EDGE STAB ST 198.23 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 186A1001 REV - P/N USED 654A0004-686; [02] REPLACED RIB LEADINGJun 25, 2021 · N7844A · Boeing 737752 · Horizontal Stabilizer, Spar/RibSDR SWAA2021072688262Bulkhead Web · cracked(CUSTOMER REQUEST) CRACK VAPOR VARRIER BST 663.75 APROX. RBL 30 AT MAIN WHEEL WELL COMPARTMENT ; 2021-296377 / [01] TOOL USED CALIPER P/N: 500-197-30; S/N: 15120583; DUE DATE: 11-FEB-22.; [02] TOOL USED HOT BONDER P/N: HCS9200B S/N: 18175478 DUE DATE 07-JUL-21Jun 25, 2021 · N7844A · Boeing 737752 · Fuselage Main, Bulkhead
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