Boeing 737-79P

Service difficulty reports · 2,376

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 = '73779P'
  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 SWAA2022013120215Seal · crackedRT WING TRAILING EDGE INBD OF DEFLECTION CONTROL RIB SEAL SUPPORT CRACKED FWD OF WEB. / REMOVED DAMAGED DEFLECTION CONTROL RIB SEAL SUPPORT FROM RT WING T/E. INSTALLED NEW SEAL SUPPORT IAW SRM 51-40-02-0G-0 PARA. 4. FASTENER CALLOUTS IAW IPC 57-50-00-25Sep 11, 2017 · N7862A · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2017101617131Web · crackedRIGHT WING TRAILING EDGE INBOARD OF DEFLECTION CONTROL RIB PANEL SUPPORT WEB CRACKED AT OUTBOARD END. R & R THE WEB IAW SRM.Sep 11, 2017 · N7862A · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2017101617130Support Angle · crackedRIGHT WING TRAILING EDGE INBOARD OF DEFLECTION CONTROL RIB PANEL SUPPORT ANGLE CRACKED. R & R THE SUPPORT ANGLE IAW SRM.Sep 11, 2017 · N7862A · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2017091816355Slide · looseL1 DOOR SLIDE LOOSE. SECURED THE SLIDE IAW MT.Sep 11, 2017 · N7857B · Boeing 73779P · Escape SlideSDR SWAA2017110617590Rib · crackedRIGHT HORIZONTAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED. R & R THE RIB IAW SRM & DWG.Sep 9, 2017 · N7862A · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2017101617078Stiffener · crackedRIGHT HORIZONTAL STABILIZER 3RD FROM FORWARD STIFFENER CRACKED AT HSS 129.50. REPAIRED THE STIFFENER IAW SRM.Sep 9, 2017 · N7862A · Boeing 73779P · Horizontal Stabilizer StructureSDR SWAA2017101617077Stiffener · crackedLEFT HORIZONTAL STABILIZER 3RD FROM FORWARD STIFFENER CRACKED AT HSS 92.70. REPAIRED THE STIFFENER IAW ER AND EA.Sep 9, 2017 · N7862A · Boeing 73779P · Horizontal Stabilizer StructureSDR SWAA2017101617076Stiffener · crackedLEFT HORIZONTAL STABILIZER 2ND FROM FORWARD STIFFENER AT HSS 92.70 CRACKED. REPAIRED STIFFENER IAW ER AND EA.Sep 9, 2017 · N7862A · Boeing 73779P · Horizontal Stabilizer StructureSDR SWAA2022013120192Plate · brokenRW PANEL 651GB I/B WIGGLE PLATE BROKEN / REMOVED RW I/B WIGGLE PLATE AND INSTALLED NEW WIGGLE PLATE FOR PANEL 651GB IAW SRM 51-40-02-0G-0 STEP 4 AND IPC 57-50-00-30.Sep 7, 2017 · N7862A · Boeing 73779P · Wing, Plate/SkinSDR SWAA2017101617075Skin · crackedLEFT WING FAIRING 542BB INNER SKIN CRACKED JUST FORWARD OF OUTBOARD AFT DRAIN HOLE. REPAIRED THE FAIRING SKIN IAW EA AND ER.Sep 7, 2017 · N7862A · Boeing 73779P · Wing Main, Frame StructureSDR SWAA2022013106692Frame · elongatedSUPPLEMENTAL INFORMATION: AFT CARGO STA. 847 FRAME HAS ELONGATED HOLE AT APPROX. LBL 20 AT AREA WHERE L/H TRANSITION ANGLE ATTACHES. / REPAIRED ELONGATED HOLE IN AFT CARGO; STATION FRAME 847; LBL 20' PER EA 1-753-31669 REV 1. SEE INDIVIDUAL WIPS AND TASKS FOR Sep 6, 2017 · N7826B · Boeing 73779P · Fuselage Main, FrameSDR SWAA2022013120172Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 221BF WITH UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH SERVICEABLE FLOOR PANEL.Sep 6, 2017 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013120173Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 221CF WITH UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH SERVICEABLE FLOOR PANEL.Sep 6, 2017 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013120174Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / DAMAGED FLOOR PANEL 221EF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9.Sep 6, 2017 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013120176Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / DAMAGED FLOOR PANEL 222BF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR 9.Sep 6, 2017 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013120177Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS SMALL AREA OF PULLED STRANDS. / REPAIRED UPPER SKIN WITH SMALL AREA OF PULLED STRANDS ON FWD FLOOR PANEL 222BF IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-2. 57066U 09/12/17Sep 6, 2017 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013120175Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS SMALL AREA OF PULLED STRANDS WITH DAMAGED INSERTS. / REPAIRED UPPER SKIN WITH SMALL AREA OF PULLED STRANDS AND REPLACED DAMAGED INSERTS ON FWD FLOOR PANEL 221DF IAW SRM 53-00-50-2R-1. 57066U 09/11/17Sep 6, 2017 · N7862A · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013106689None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS SURFACE CORROSION AROUND FASTENER HOLES IN BETWEEN STA.727A AND STA. 807. / REMOVED AND REPLACED L/H TRANSITION ANGLE PER SRM 51-40-02Sep 5, 2017 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022013106690Strip · corrodedAFT CARGO R/H TRANSITION ANGLE HAS SURFACE CORROSION AROUND FASTENER HOLES IN BETWEEN STA.727A AND STA. 767. / E105618-BLACKBURN; RICHARD - 09/07/2017 22:40 COMPLETE: REMOVED DAMAGED R/H TRANSITION ANGLE AND INSTALLED NEW SERVICEABLE R/H TRANSITION ANGLE FROM Sep 5, 2017 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022011906681Floor Panel · corrodedFWD CARGO FLOOR PANEL 120AF DENTED AND HAS CORROSION. / REMOVED AND REPLACED FLOOR PANEL 120AF IAW AMM 25-52-10.Aug 31, 2017 · N7826B · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022020119398Scuff Plate · crackedFWD CARGO BAY CENTER SCUFF PLATE HAS SEVERAL CRACKS ALONG I/B EDGE / PROCURED NEW FWD CARGO BAY CENTER SCUFF PLATE P/N #143A8333-8 P.O #645119. THIS CARD FOR PARTS TRACKING ONLYAug 29, 2017 · N7860A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022020119399Scuff Plate · crackedFWD CARGOBAY FWD SCUFF PLATE IS CRACKED / FWD CARGO BAY FWD SCUFF PLATE REPAIRED PER EA 1-A53-2076 REV II 41250U 01SEPT17Aug 29, 2017 · N7860A · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022020106659Scuff Plate · crackedAFT CARGO FWD SCUFF PLATE CRACKED / REMOVED AND REPLACED PER TASK CARD 753-721-10-01Aug 27, 2017 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022020106660Scuff Plate · crackedFWD CARGO FWD CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED IAW SRM 51-40-02.Aug 27, 2017 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022020106661Scuff Plate · crackedFWD CARGO AFT CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED IAW SRM 51-40-02.Aug 27, 2017 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022020106663Plate · crackedWAFFLE PLATE IS CRACKED; RIVET SHEARED ABOVE LEFT AFT STRUT FAIRING AT ORSS 261(MARKED). / REMOVED AND REPLACED WAFFLE PLATE ABOVE LEFT AFT STRUT FAIRING AT ORSS 261 PER SRM 51-40-02Aug 27, 2017 · N7826B · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2022020106665Plate · crackedWAFFLE PLATE IS CRACKED; RIVET SHEARED ABOVE LEFT AFT STRUT FAIRING AT ORSS 261(MARKED). / REMOVED AND REPLACED WAFFLE PLATE ABOVE LEFT AFT STRUT FAIRING AT ORSS 261 PER SRM 51-40-02Aug 27, 2017 · N7826B · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2022020106655Scuff Plate · crackedAFT CARGO ENTRY AFT CORNER SCUFF PLATE HAS A CRACK AT AFT SIDE. / REMOVED AND REPLACED PER TASK CARD 753-721-10-01Aug 26, 2017 · N7826B · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022020119395Plate · crackedL/W T/E ORSS 261 WIGGLE PLATE IS CRACK. / REMOVED DAMAGED L/W T/E WIGGLE PLATE AT ORSS 261. INSTALLED NEW WIGGLE PLATE IAW SRM 51-40-02-0G-0 STEP 4 AND DWG #115A2001.Aug 26, 2017 · N7860A · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2022011906650Floor Panel · crackedAFT CARGO FLOOR PANEL 140CF HAS A CRACK AND SEVERAL DENTS. / REMOVED AND REPLACED FLOOR PANEL IAW AMM 25-52-10.Aug 26, 2017 · N7826B · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022020119866Angle · cracked(RIGHT WING) T/E COVE SEAL RETAINING ANGLE CRACKED ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED RIGHT WING T/E COVE SEAL RETAINING ANGLE ABOVE #2 PYLON AFT TIP. IAW. SRM 51-40-02.Aug 23, 2017 · N7861J · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2022020119792Plate · crackedLW LOWER FIXED TRAILING EDGE WIGGLE PLATE CRACKED JUST IB OF #1 PYLON TAILCONE / REMOVED AND REPLACED L/W LOWER FIXED T/E WIGGLE PLATE I/B OF #1 PYLON PER S.R.M. 51.40.02.0G.0 STEPS 4.B. AND PER BOEING DWG 115A2001Aug 21, 2017 · N7861J · Boeing 73779P · Wing Miscellaneous StructureSDR SWAA2022013119710Floor Panel · corrodedFCB FLOOR PANEL 120BF IS CORRODED / APPLICABILITY STATEMENT IAW SRM 53-30-53-01-1 FOR ID AND SRM 53-00-53-1A-1 FOR ALLOWABLE DAMAGE ARE APPLICABLE. REMOVED CORROSION ON AREA OF 12' X 2' X .010 ORIGINAL THICKNESS .071 FOUND TO BE OUT OF LIMITS IAW SRM 53-0053-1Aug 16, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013119711Floor Panel · corrodedFCB FLOOR PANEL 120CF IS CORRODED / FABRICATED FORWARD CARGO FLOOR PANEL 120CF OUT OF 0.071 2029 T3 CIAD ITEM #2024T3 #0.071 LOT #1291186 IAW AMM 25-52-01-201-801 & BOEING DRAWING #453A1610. APPLIED CHEMICAL COVERSION COATING AND PRIMER PER AMM 51-21-41-370-80Aug 16, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013119713Floor Panel · corrodedACB FLOOR PANEL 140AF IS CORRODED / OK TO APPLY CHEMICAL COVERSION COATING & PRIMER. FABRICATED ACB FLOOR PANEL 140AF OUT OF 0.071 2024T3 CIAD ITEM #2024T3# 0.071 X 48 SH-C LOT #1301872-1 IAW AMM 25-52-01-201-801 & BOEING DRAWING #4533A2610. 57006U 08SEP17 LEAAug 16, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013119714Floor Panel · corrodedACB FLOOR PANEL 140BF IS CORRODED / FABRICATED NEW FLOOR PANEL #140BF IAW SRM 53-60-53- 0I-1;SRM 51-40-05 AND DWG 453A2610. PRIOR TO FABRICATING PANEL; EVALUATED PANEL 140BF PER SRM 53-00-53-1A-1 PAR 5.A(1)(6) AND FOUND IT TO BE OUT OF LIMITS DUE TO MORE THEN Aug 16, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013119715Floor Panel · corrodedACB FLOOR PANEL 140DF IS CORRODED / FABRICATED.NEW FLOOR PANEL #140DF IAW.SRM 53-70-53- 0I-1 SRM 51-40-05 AND DWG 453A2610. PRIOR TO FABRICATING PANEL; EVALUATED PANEL 140DF PER SRM 53-00-1A-1 PARAGRAPH 5 (A)(1)(B) AND FOUND IT TO BE OUT OF LIMITS DUE TO MORE Aug 16, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019687Floor Panel · pulledFWD CABIN FLOOR PANEL 221BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221BF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.Aug 15, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019688Floor Panel · pulledFWD CABIN FLOOR PANEL 221CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221CF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.Aug 15, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019690Floor Panel · pulledFWD CABIN FLOOR PANEL 221EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221EF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.Aug 15, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019689Floor Panel · pulledFWD CABIN FLOOR PANEL 221DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221DF WITH UPPER SKIN HAVING MULTIPLE AREASOF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.Aug 15, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019691Floor Panel · pulledFWD CABIN FLOOR PANEL 221FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221FF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.Aug 15, 2017 · N7891J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019692Floor Panel · pulledFWD CABIN FLOOR PANEL 221GF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221GF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.Aug 15, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019693Floor Panel · pulledFWD CABIN FLOOR PANEL 222CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 222CF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.Aug 15, 2017 · N7861J · Boeing 73779P · Fuselage Floor PanelSDR SWAA2022013019696Floor Support · crackedFLOOR SUPPORT CRACKED AT BS-540; RBL-23; WL-207. / REMOVED AND REPLACED FLOOR SUPPORT AT BS 540 BL-0 TO RBL-25 WL 207 IAW SRM 51-40-02-0G-0 56208U 20AUG17 AND BOEING DWG D.R #143A0060 REV AAug 15, 2017 · N7861J · Boeing 73779P · Fuselage Miscellaneous StructureSDR SWAA2022013019698None · corroded***CORROSION*** ON L/H MOPSILL; BS-302 TO BS-348; WL-207 / REMOVED AND REPLACED L/H FWD MOPSILL PER SRM 51-40-02 & DWG #141A8110Aug 15, 2017 · N7861J · Boeing 73779P · Fuselage Main, Plate/SkinSDR SWAA2022013019686Rib · crackedRT HORIZONTAL STAB IN SPAR RIB AT 92.70 IS CRACKED ON THE LOWER END OF THE 4TH VERTICAL STIFFENER FROM THE FRONT. / REPAIRED RT. HORIZ. STAB IN-SPAR RIB AT 92.70 ON LOWER END OF THE 4TH VERTICAL STIFFENER FROM THE FRONT IAW EA 1-755-3795 REV IR AND ER 17-03850Aug 15, 2017 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2022013019685Rib · crackedRT HORIZONTAL STAB IN SPAR RIB AT 92.70 IS CRACKED ON THE LOWER END OF THE 3RD VERTICAL STIFFENER FROM THE FRONT. / REMOVED CRACK DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4Aug 15, 2017 · N7861J · Boeing 73779P · Horizontal Stabilizer, Spar/RibSDR SWAA2022013019678Scuff Plate · corrodedL/H AFT MOP SILL IS CORRODED / LOCATED AND DRILLED NEW MOPSILL AT AFT ENTRY DOOR IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02 AND DWG 147A8501 88324U 23AUG17Aug 13, 2017 · N7861J · Boeing 73779P · Fuselage Main, Plate/SkinSDR SWAA2022013019679Scuff Plate · corrodedR/H AFT MOP SILL IS CORRODED / LOCATED AND DRILLED NEW MOPSILL AT AFT SERVICE DOOR IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02 AND DWG 147A8501 88324U 22AUG17Aug 13, 2017 · N7861J · Boeing 73779P · Fuselage Main, Plate/Skin
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