Boeing 737-76N

Service difficulty reports · 4,807

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 = '73776N'
  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 SWAA2021081095246Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500A+2 TO 500C+15 RBL 25 WL 156 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500A+2 - BS500C+15'; RBL25; WL 156 PER SRM51-10-02-0G-0 MEASURE L=59'X W=1'X D=0.006' MAX. MAT LOSS IS 0.00Jul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095292Strap · corrodedCORROSION ON STRAP AT AFT CARGO BAY BS809 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTED Jul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095294Strap · corrodedCORROSION ON STRAP AT AFT CARGO BAY BS820 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTED Jul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095295Strap · corrodedCORROSION ON STRAP AT AFT CARGO BAY BS824 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTED Jul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095308Strap · corrodedCORROSION ON STRAP AT AFT CARGO BAY BS816.5 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1'; W=1'; [03] UT INSPECTEJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095265Web · corrodedCORROSION ON FWD CARGO BAY SUB THRESHOLD WEB BS 464 RBL 28 WL 156 ; / [01] REMOVAL CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB BS 464 RBL 28 WL 156 ; MEASURES L=2.5' X W= 1.8' X D=0.018' MAX MAT LOSS IS 0.018' REMAINING THICKNESS 0.027' FOUND OUT OF LIMITS REJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095274Intercostal · corrodedCORROSION ON INTERCOSTAL AT AFT CARGO BAY BS847 RBL23 WL163. ; / REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9; [02] REMOVED INTERCOSTAL AT AFT CARGO BAY BS847 RBL23 WL163. THIS PART DOES NOT HAVE ENTRY ON THE LOWER DAMAGED THERE FOR IT HAS TO BE REPAIRED BYJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095284Frame Splice · corrodedCORROSION ON FRAME SPLICE AT AFT CARGO BAY BS767 RBL25 WL157. ; / [01] DAMAGE FOUND AT ACB FRAME SPLICE BS-767 RBL-25 WL-157 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-O PAR.9C; [02] VERIFIED DAMAGEJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Main, FrameSDR SWAA2021081095286Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS773 RBL20 WL157. ; / [01] REMOVED CORROSION ON ACB WEB BS 773 RBL 20 WL 157 IAW SRM 51-10-02-0G-0; EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1; PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARTJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095288Frame Splice · corrodedCORROSION ON FRAME SPLICE AT AFT CARGO BAY BS787 RBL25 WL158. ; / REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-O PAR.9C; [02] VERIFIED DAMAGE FOUND AT ACB FRAME SPLICE BS-787 RBL-25 WL-158 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BYJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Main, FrameSDR SWAA2021081095291Strap · corrodedCORROSION ON STRAP AT AFT CARGO BAY BS787+17 RBL19 WL159. ; / [01] REMOVED CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1 W=1; [02] VERIFIED REMOVAL OF CORROSION ON STRAP AT AFT CARGO BAY PER REF SRM 53-60-15-1A-1 L=1' W=1'; [03] UT INSPECTEJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095307Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS802 - BS827 RBL26 WL159. ; / [01] REMOVED CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS802-BS827 RBL26 WL159 DIMENSIONS: L=25' W=2' D=0.007' WAS FOUND OUT OF LIMIT DUE MATERIAL LOSS IS MORE THAN 10% OF THICKJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095290Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS792 RBL19 WL157. ; / [01] REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 792 RBL 19 WL 157 MAX MATERIAL LOSS L=4';W=1';D=0.020 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 STEP 4G (2)(B) FIG 103 TOOL USED ID ATS1672 S/N 650Jul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095270Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS873 - BS887 RBL21 WL169. ; / [01] REMOVED CORROSION AT FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 873 BS 887 RBL 21 WL 169 MAX MATERIAL LOSS L=5';W=2.5';D=0.006' FOUND TO BE OUT OF LIMITS IAW SRM 53-Jul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095253Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 441 TO 458 LBL 24 WL 156 ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 400+6'; LBL24; WL 156 PER SRM51-10-02-0G-0 MEASURE L=1'X W=0.75'X D=0.006' MAX. MAT LOSS IS 0.006'; REMAINING THICJul 15, 2021 · N7723E · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021081095240Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] CUT 0UT AND REMOVED DAMAGED SECTION AT VERTICAL STIFFENER OF THE RIB L= .80; W=.312 STATION 129.50 3RD VERTICAL STIFFENER PER SRM 55-10-09-2RJul 15, 2021 · N7723E · Boeing 73776N · Horizontal Stabilizer StructureSDR SWAA2021081095239Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] PERFORMED CUT OUT 3RD VERTICAL STIFFENER STAB INSPAR RIB AT STA 129.50 L: .900' W: .312' IAW SRM 55-10-09-2R-4 REPAIR 4; [02] REQ NDI CUT OUT Jul 15, 2021 · N7723E · Boeing 73776N · Horizontal Stabilizer StructureSDR SWAA2021081095229Pressure Deck · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] DAMAGED AT EXISTING REPAIR FOUND TO BE OUT OF LIMITS NO ALLOWABLE DAMAGE FOUND AT SRM; [02] ADDING SRM REFERENCE USED: SRM 53-10-51-1A-1; [03] CORRECTING MEASUREMENT FOR SHORTJul 14, 2021 · N7723E · Boeing 73776N · Fuselage Main, StructureSDR SWAA2021081097224Skin · dentedFUSELAGE EXTERNAL SKIN HAS A DENT AT BS 500C+9'; 2.3' ABOVE STR 5R. ; / [01] REMOVED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA TO FOM PER AMM 51-21-11; [02] EVALUATED DENT AT DISCREPANCY AREA L= 1.5' W=1.3' FOUND TO BE OUT OF LIMITS DUE TO BLEND OUT (AREA Jul 13, 2021 · N7723E · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2021081094322Skin · corrodedFUSELAGE EXTERNAL SKIN HAS A CORROSION AT 1089 BETWEEN STR 18LH- STR 21LH ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED CORROSION AT DISCREPANCY AREA PER REF SRM 51-10-02-0G-004] ET INSPECTED BLEND/HOLES/COUNTERSINKS IAW 737 NDTJul 13, 2021 · N7723E · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2021081094328Skin · corrodedFUSELAGE EXTERNAL SKIN HAS CORROSION AT BS 1089 AROUND PRIMARY JACK POINT 'C' ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED CORROSION AT DISCREPANCY AREA L=3.7' W=2.7' PER SRM 51-40-02; [03] STEP 2 REFERENCE ENTRY AND ERROR. REMJul 13, 2021 · N7723E · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2021081094320Skin · corrodedFUSELAGE AFT SKIN PANEL AT BUTT JOINT BS 1016 HAS CORROSION BETWEEN STR 21L - 22L ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED FASTENERS AT DISCREPANCY AREA PER REF SRM 51-40-02; [03] REMOVED CORROSION AT DISCREPANCY AREA PER SJul 13, 2021 · N7723E · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2021081094323Skin · corrodedFUSELAGE AFT SKIN PANEL AT BUTT JOINT BS 1016 HAS CORROSION BETWEEN STR 24L - 24R ; / [01] REMOVED PAINT AT DISCREPANCY AREA PER REF AMM 51-21-11; [02] REMOVED CORROSION AT DISCREPANCY AREA PER REF SRM 53-00-01-1A-1; [03] REMOVED 11EA FASTENERS AT BLENDED AREAJul 13, 2021 · N7723E · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2021081094292Skin · crackedCRACK IN #5 SLAT LOWER SKIN NEAR ACTUATOR FITTING ATTACH FASTENER ; / [01] HFEC INSPECTED CRACK ON #5 SLAT LOWER SKIN IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; AREA MARKED. EQUIP ID#: IS000450 S/N: N500D000M120071; [02] REMOVED HI LOCK AT #5 SLAT LOWER SKIN NJul 12, 2021 · N7723E · Boeing 73776N · Leading Edge DevicesSDR SWAA2021070890586Battery · faultyUPR & LWR FWD EMER FLASHLIGHTS NOT BLINKING ; / [01] R&R BOTH UPR AND LWR FWD EMER FLASHLIGHT BATTERIES PER AMM 25-64-00Jul 4, 2021 · N7811F · Boeing 73776N · Emergency EquipmentSDR SWAA2021063088208Link · crackedRIGHT MLG SUPPORT BEAM ;LOWER O/B STABILIZER LINK CRACKED APPOX 1 INCH LONG . CRACK IS LOCATED AT FWD SIDE LUG NEAR ATTACHMENT POINT. ; / [01] REMOVED AND REPLACED THE R/H MLG SUPPORT BEAM LOWER STABILIZER LINK REF AMM 57-15-00Jun 26, 2021 · N7822A · Boeing 73776N · Main Landing GearSDR SWAA2021062888299Sensor · faultyON APPROACH SELECTED FLAPS 5; FLAPS LOCKED AT 2 ; ON APPROACH INTO ABQ ; SELECTED FLAPS 5 ; FLAPS MOVED TO POSITION 2 ; RAN FLAPS ; TRAILING EDGE DISAGREE QRH. PER QRH USED ALT FLAPS SWITCH TO POSITION TRAILING EDGE FLAPS TO 15; LANDED NORMALLY / [01] REMOVED Jun 26, 2021 · N7846A · Boeing 73776N · Trailing Edge Flap Control SystemSDR SWAA2021062185312Wedge · debondedRIGHT WING INBOARD MAIN FLAP LOWER SKIN DISBONDED ON TRAILING EDGE AT OUTBOARD END. REMOVED TE WEDGE IAW SRM 51-40-02-0G-0 VERIFIED RT INBD FLAP WEDGE PART EFFECTIVITY . INSTALLED NEW RIGHT WING I/B FLAP AFT WEDGE ASSEMBLY IAW DWG 113A2100 REV A AND PL 113AJun 16, 2021 · N7846A · Boeing 73776N · Trailing Edge FlapsSDR SWAA2021061582602Support Fitting · corrodedRT MLG FWD TRUNNION SUPPORT FITTING ; RT MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG; I/B FACE HAS EVIDENCE OF CORROSION / REPAIRED AS PER EA-1-A57-3246 REV 12Jun 12, 2021 · N7822A · Boeing 73776N · Wing, Landing Gear Attach FittingsSDR SWAA2021060278243Cover · missingR1 DOOR SLIDE LENSE COVER MISSING REF LP# 1811387 MEL 25-10-01 AUTH# 13799 ; / INSTALLED R1 DOOR SLIDE COVER PER AMM 20-30-11.May 29, 2021 · N7822A · Boeing 73776N · Escape SlideSDR SWAA2021060278152Lens · brokenEMERGENCY EXIT LIGHT COVER PLATE LENS DOOR L1 BROKEN ; / REINSTALLED LENS IAW SIPMay 29, 2021 · N7731A · Boeing 73776N · Emergency LightingSDR SWAA2021061480210Skin · dentedDENT EXTERNAL SKIN LOCATED BETWEEN STA 219.5 TO STA 224.8 AND ABOVE S-24L FUSELAGE EXTERIOR ; 2021-217461 / EA # 21-153-01510 COMPLETED; EA # 21-153-01510 COMPLETED RII; EA # 21-153-01510 COMPLETED RIIMay 24, 2021 · N7818L · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2021061480205Skin · dentedDENT EXTERNAL SKIN LOCATED BETWEEN STA 219.5 TO STA 224.8 AND ABOVE S-24L FUSELAGE EXTERIOR ; 2021-217461 / PERFORMED REPAIR IAW EA # 21-153-01510-WIP1 AND EA# 21-153-01510; PERFORMED REPAIR IAW EA # 21-153-01510-WIP1 AND EA# 21-153-01510 RII; PERFORMED REPAIRMay 24, 2021 · N7818L · Boeing 73776N · Fuselage Main, Plate/SkinSDR SWAA2021062178888Floorbeam · crackedCRACK IB HOLE ON LOWER CHORD LONGITUDINAL FLOOR BEAM RBL 45.57 AT BS663 CENTER PASSENGER CABIN ; 2021-229906 / TOOL P/N:NORTEC 500D; S/N: N500X12101V022240; CAL DUE: 01-DEC-21. COMPLETED EA# 21-153-01516-WIP1May 22, 2021 · N7811F · Boeing 73776N · Fuselage Main, Floor BeamSDR SWAA2021062180203Floorbeam · crackedCRACK IB HOLE ON LOWER CHORD LONGITUDINAL FLOOR BEAM RBL 45.57 AT BS663 CENTER PASSENGER CABIN ; 2021-229906 / TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 08-OCT-21. REPAIRED LOWER CHORD LOWER LONGITUDINAL FLOOR BEAM RBL 45.57 AT BS 663 CENTEMay 22, 2021 · N7811F · Boeing 73776N · Fuselage Main, Floor BeamSDR SWAA2021061875759Floorbeam · crackedCRACK IB HOLE ON LOWER CHORD LONGITUDINAL FLOOR BEAM RBL 45.57 AT BS663 CENTER PASSENGER CABIN ; 2021-229906 / REPAIRED LOWER CHORD LOWER LONGITUDINAL FLOOR BEAM RBL 45.57 AT BS 663 CENTER PASSENGER CABIN IAW EA# 21-153-01516 BARCODE TTG8Q005FNBT; EA# 21-153-0May 22, 2021 · N7811F · Boeing 73776N · Fuselage Main, Floor BeamSDR SWAA2021061475488Support Angle · crackedCRACK ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 3 AT LT WING (1 EA) ; 2021-217453 / REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 3 AT LT WING (1 EA) IAW B737-700. SRM 51-40-02.; REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIARMay 21, 2021 · N7818L · Boeing 73776N · Wing Miscellaneous StructureSDR SWAA2021061475487Support Angle · crackedCRACK ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 6 AT RT WING (1 EA) ; / REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INBOARD SLAT 6 AT RT WING (1E/A) IAW B737-700 SRM 51-40-02-0G-0; REPLACED ANGLE SUPPORT OF COVER PLATE AUXILIAR TRACK INMay 21, 2021 · N7818L · Boeing 73776N · Wing Miscellaneous StructureSDR SWAA2021062175479Stringer Clip · crackedCRACK TIE CLIP BS360 STR 8R AT PASSENGER CABIN ; 2021-229867 / REPLACED TIE CLIP LOC. BS 360 STR 8R AT PASSENGER CABIN.IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG # 140A9111 REV-C.; REPLACED TIE CLIP LOC. BS 360 STR 8R AT PASSENGER CABIN.IAW B737-700 SRM 51-40May 20, 2021 · N7811F · Boeing 73776N · Fuselage Main, Attach FittingsSDR SWAA2021061475486Angle · crackedCRACK ANGLE LOCATED ON BS 420 AND STRINGER 26L AT FWD CARGO COMPARTMENT ; 2021-217404 / REPLACED ANGLE LOCATED ON BS 420 AND STRINGER 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 143A7505 REV :B; REPLACED ANGLE LOCATED ON BS 420 May 20, 2021 · N7818L · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021061475485Web · crackedCRACK ON WEB LOCATED BETWEEN BS 400 TO BS 420 AND STRINGER 26L FWD CARGO COMPARTMENT ; 2021-217403 / REPLACED WEB LOCATED BETWEEN BS 400 TO BS 420 AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A7505 REV: B; REPLACED WEMay 20, 2021 · N7818L · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021052474531Battery Pack · no testEMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675 ; / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M01675 PER AMM 33-51-06May 19, 2021 · N7822A · Boeing 73776N · Emergency LightingSDR SWAA2021052474162Seal · bentLEFT HORIZONTAL STABILIZER LOWER SLIDING SEAL BENT ; /May 18, 2021 · N7822A · Boeing 73776N · Horizontal Stabilizer StructureSDR SWAA2021052474161Seal · crackedLEFT HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED ; /May 18, 2021 · N7822A · Boeing 73776N · Horizontal Stabilizer StructureSDR SWAA2021062174527Frame · crackedCRACK FRAME LOCATED BS 360 BETWEEN STRINGER 8R / 9R AT PASSENGER CABIN ; 2021-229793 / TASK CARD COMPLETE.; TASK CARD COMPLETE AND CERTIFIED AS RII.; TASK CARD COMPLETE AND CERTIFIED AS RII. REPAIRED FRAME ON BS 360 BTW STR 8R/9R AT PASSENGER CABIN IAW EA# 1-AMay 15, 2021 · N7811F · Boeing 73776N · Fuselage Main, FrameSDR SWAA2021062173405Angle · corrodedCORROSION Z ANGLE LOCATED BETWEEN BS 294.5 TO BS 328 AT LEVEL STRINGER 17R AT FWD GALLEY AREA ; 2021-229807 / INSTALLED Z ANGLE AND FASTENERS LOCATED BETWEEN BS 294.5 TO BS 328 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG # 141A83May 15, 2021 · N7811F · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021062173404Web · crackedCRACK WEB LOCATED BETWEEN BS 277 TO BS 294.5 AND BL 0 AT FWD GALLEY AREA ; 2021-229804 / REPLACED WEB AND LOCATED BTW BS277 TO BS294.5 AND BL0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 STEP 9. PART NUMBER USED 141A5410U139;REPLACED WEB LOCATED BTW BS27May 15, 2021 · N7811F · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021061873403Frame · crackedCRACK FRAME LOCATED BS 360 BETWEEN STRINGER 8R / 9R AT PASSENGER CABIN ; 2021-229793 / REPAIRED FRAME ON BS 360 BTW STR 8R/9R AT PASSENGER CABIN IAW EA# 1-A53-12114; TASK CARD COMPLETE AND CERTIFIED AS RII.; TASK CARD COMPLETE AND CERTIFIED AS RII.May 15, 2021 · N7811F · Boeing 73776N · Fuselage Main, FrameSDR SWAA2021062173388Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 947.5 STRINGER 26L AT AFT CARGO COMPARTMENT ; 2021-229767 / REPLACED ANGLE-SUPPORT LOCATED ON BS947.5; STRG26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG #149A8103; SHEET: 6; REV: -; PART USMay 14, 2021 · N7811F · Boeing 73776N · Fuselage Miscellaneous StructureSDR SWAA2021062173380Stringer Clip · crackedCRACK TIE CLIP LOCATED BS 277 AT LEVEL STRINGER 10R AT PASSENGER CABIN ; 2021-229762 / REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STRINGER 10R AT PASSENGER CABIN; PART USED: 141A1250U92 I.A.W. B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02 AND DWG 141A111May 14, 2021 · N7811F · Boeing 73776N · Fuselage Main, Attach Fittings
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