JASC 5350

Service difficulty reports · 6,121

Reports filed under 5350 · Aerodynamic Fairings, newest first.

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 jasc_code = '5350'
  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 SWAA2023050116652Panel · crackedLOWER FUSELAGE ACCESS PANEL 193D LOWER SKIN SURFACE HAS CRACKS AT SEVERAL FASTENER HOLES. (18-021)<[01] RECIEVED NEW PART# 149A7653-5 PO# 2012626. REF TASK TTG8Q00HL105 FOR PANEL INSTALLATION;[02] VERIFIED STEP 1.Mar 15, 2023 · N7858A · Boeing 73779PSDR VNAA202304270032Retainer · corrodedCORROSION ON SEAL RETAINER OF LH/RH WING TO FUSELAGE FAIRING AT WHEEL WELL AREA.Mar 14, 2023 · N619NN · Cndair CL6002D24SDR SWAA2023032415376Bracket · crackedFOUND PANEL SUPPORT BRACKET CRACKED AT STA 500L BEHIND PANEL 191AR<[01] REMOVED PANEL 191AR FOR ACCESS TO BRACKET REF B737-700 SRM 51-40-02-0G-0;[02] REMOVED R/H SUPPORT BRACKED AT STA 500L IN REF TO B737 AMM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW SUPPORT Mar 12, 2023 · N936WN · Boeing 7377H4SDR SWAA2023041113471Fairing · crackedCRACK ACCESS PANEL 194FL APU SHROUD AND HYDRAULIC DRAIN AT LOWER FUSELAGE 2023-180813<[01] REMOVED AND REPLACED FOR A SERVICEABLE SHROUD AND HYDRAULIC DRAIN AT LOWER FUSELAGE ON ACCESS PANEL 194FL P/N:346A2801-5 AND S/N:SN036230 IAW B737-700 AMM 28-25-07-020-8Mar 7, 2023 · N280WN · Boeing 7377H4SDR SWAA2023033012272Panel · chafedPANEL 194AR MATING SURFACE IS CHAFED.<[01] IDENTIFIED 194AR PANEL IAW SRM 53-60-70-0I-1 PARA FIGURE 2; ITEM 1; TABLE 2<BR><BR>FOUND DAMAGE TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA 4.B.(8).<BR><BR>WILL PERFORM WORK IAW SRM 53-60-70-1A-1 PARA 2.AMar 4, 2023 · N7819A · Boeing 7377Q8SDR IPXA2023032192095Frame · elongatedINSPECTION TYPE:3CTAIL CONE AFT UPPER HINGE FITTING FOUND FRAME ELONGATED ON UPPER SIDE.REMOVED, FABRICATED AND REPLACED FRAME AT TAIL CONE AFT UPPER SIDE IAW SRM 51-35-01 AND 51-33-01 (MINOR)Mar 3, 2023 · N294UP · Doug MD11FSDR SWAA2023031309869Panel · delaminatedWTB FAIRING 193AL DELAMINATED<[01] REMOVED DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES AT ACCESS PANEL WTB FAIRING 193AL. NO WATER NOTE AT REPAIR AREA. REF B737 SRM 51-70-04-2R-13 PARAGRAPH 4.;[02] VERIFIED STEP 1. OK TO APPLFeb 24, 2023 · N277WN · Boeing 7377H4SDR AALA202304046621Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SKIN OF ZONE 191 LOWER WING TO BODY FAIRING, FORWARD OF WING BOX, LOCATED FROM BS 727D TO BS 727F AND FROM S23L TO S26L. REPAIRED SKIN PER EA 343136 AND SRM 51-10-02-0G.Feb 19, 2023 · N923AN · Boeing 737823SDR SWAA2023032005046Fairing · crackedR/H OVERWING FAIRING 195CR FWD LOWER SECTION HAS A CRACK.<[01] PERFORMED VISUAL INSPECTION AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL PER B737 NDTM 51-05-01;[02] PREPARED DAMAGED AREA AT PANEL #195CR FOR REPAIR PER B737 SRM 51-70-04-2R-Feb 19, 2023 · N8664J · Boeing 7378H4SDR SWAA2023022104594Fairing · cracked#2 ENGINE PYLON AFT. STRUT SUPPORT FAIRING ASSY. IS CRACK<[01] DRILLED UP NEW PYLON AFT; STRUT SUPPORT FAIRING ASSY. PER SRM 51-40-05.;[02] INSTALLED NEW STRUT SUPPORT FAIRING PER SRM 51-40-02Feb 18, 2023 · N8567Z · Boeing 7378H4SDR SWAA2023022409007Plate · missingPANEL 561AB IS MISSING WIGGLE PLATE.<[01] REPLACED MISSING WIGGLE PLATE AT LEFT WING AT ACCESS PANEL #561AB AS PER B 737 SRM 51-40-02-0G-0 AND INSTALLATION DWG 115A3712.;[02] VALIDATED STEP 1;[03] PERFORMED BOUNDING TEST TO FASTENERS AS PER B 737 SWPM 20-20-10Feb 15, 2023 · N408WN · Boeing 7377H4SDR SWAA2023031303241Panel · debondedWING TO BODY FAIRING PANEL 191CL HAS A DISBOND<[01] IDENTIFIED PANEL 191CL IAW SRM 53-30-70-0I-1 FIGURE 2 ITEM [8]. BEFORE SANDING AWAY THE PAINT LAYERS IN DISCREPANT AREA; TAP TESTED THE DISCREPANT AREA IAW SRM 53-30-70-1A-1 PARAGRAPH 2.A.(1).(A) WITH NO DISBFeb 14, 2023 · N289CT · Boeing 7377H4SDR SWAA2023030103304Angle · crackedLEADING EDGE ATTACH ANGLE FOR WING TO BODY PANEL 191AR IS CRACKED<[01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-00.;[02] DRILLED NEW ANGLE IAW SRM 51-40-02-0G-00 AND BOEING DRAWING 116A3110.;[03] VERIFIED ACTIONS 1 AND 2;[04] VERIFIED STEPS AND OK TO INSTALL;Feb 14, 2023 · N231WN · Boeing 7377H4SDR SWAA2023031302329Panel · delaminatedDELAMINATED ACCESS PANEL 193AR AT LOWER FUSELAGE 2023-113052<[01] TOOL USED: CALIPER PN: 500-197-30 B20189526 DUE DATE: 20/DEC/23.;[02] TOOL USED HOT BONDER P/N: HCS9200B P/N: 18165044; DUE DATE: 28-FEB-23;[03] TOOL USED: SCALE PN: SPX621; SN: 8340225441; DUE Feb 12, 2023 · N219WN · Boeing 7377H4SDR SWAA2023021501927Radome · crackedDURING INTERNAL DVI ON NOSE RADOME FOUND A 3 CRACK AT THE 10 O CLOCK POSITION LOOKING FROM AFT.<[01] REMOVED 14 OUT OF 16 RADOME BOLTS.;[02] R/R NOSE RADOME PER AMM 53-52-00.Feb 11, 2023 · N7822A · Boeing 73776NSDR YENA2023021400170None · noneDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR55 AND FR56 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1176129 TASKCARD: NR-00027 ) ALL WORK ACCOMPLISHED REF AEROMAN NRC 2022-676486. REMOVED AND REPLACED STFeb 10, 2023 · N508JL · Airbus A320232SDR YENA2023021400169None · noneDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR57 AND FR58 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1176129 TASKCARD: NR-00028 ) ALL WORK ACCOMPLISHED ON AEROMAN NR 2022-676482, REMOVED AND REPLACED STRINFeb 10, 2023 · N508JL · Airbus A320232SDR SWAA2023021501114Panel · elongatedPANEL 193B HAS MULTIPLE ELONGATED FASTENER HOLES<[01] REPAIRED PER SRM 51-70-04-2R-9.Feb 9, 2023 · N8609A · Boeing 7378H4SDR GTIA2023020136962Unknown · corrodedCORROSION FRAME 70 FWD FACE OF THE REAR PRESSURE BULKHEAD AT LEVEL STR 43R IN AFT CARGO COMPARTMENT-REPLACED REAR PRESSURE BULKHEAD FR 70 LOWER DOME IAW EA # 53-0643-22 AND EC NO. EO 5351-2311. REPAIR CATAGORY "A" AND INSPECTION NOT REQUIRED.Feb 9, 2023 · N605NK · Airbus A320232SDR SWAA2023032000354Panel · crackedLH UNDERWING ACCESS PANEL 192HL LOWER SURFACE AROUND FASTENER HOLE HAS MATERIAL CRACKED.<[01] PREPARED FOR REPAIR PANEL 192HL; AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED PANEL 192HL; AS PER B737 SRM 51-70-06-2R-9 MATEFeb 8, 2023 · N216WR · Boeing 7377H4SDR DALA2023020700918Not Reported · not reportedSHIP 1200 WORN SIGN FOUND ON THE SECTION 48 LH SIDE H/STAB TO FUSELAGE LOWER CUTOUT FWD SIDE LOWER SEAL FAIRING SKIN AT STA 1725. CORRECTIVE ACTION: DAMAGED AREA REPAIRED THE WORN SKIN AS PER B767-300 SRM 53-80 (2615422)Feb 5, 2023 · N1200K · Boeing 767332SDR DALA2023020700917Not Reported · not reportedSHIP 1200 WORN SIGN FOUND ON THE SECTION 48 RH SIDE H/STAB TO FUSELAGE LOWER CUTOUT FWD SIDE LOWER SEAL FAIRING SKIN AT STA 1725. CORRECTIVE ACTION: DAMAGED AREA REPAIRED THE WORN SKIN AS PER B767-300 SRM 53-80 (2615416)Feb 5, 2023 · N1200K · Boeing 767332SDR SWAA2023020798887Panel · delaminatedRIGHT WING PANEL 191FR LEADING EDGE LOWER CORNER DELAMINATION - (REF TTG8Q00GRBM3)<[01] PERMANENTLY REPAIRED PER SRM 53-30-70-2R-1 AND SRM 51-70-05-2R-0.Feb 4, 2023 · N8569Z · Boeing 7378H4SDR SWAA2023032098617Panel · corrodedCORROSION ACCESS PANEL 191CR PLATE CUT OUT OF DRAIN MAST AT LOWER FUSELAGE 2023-106128<[01] REPLACED ACCESS PANEL 191CR PLATE CUT OUT OF DRAIN MAST AT LOWER FUSELAGE I.A.W B737-700 SRM 51-40-02;[02] REPLACED ACCESS PANEL 191CR PLATE CUT OUT OF DRAIN MAST AT LOFeb 3, 2023 · N566WN · Boeing 7377CTSDR SWAA2023032098620Panel · corrodedCORROSION ACCESS PANEL 191CR DRAIN MAST AT LOWER FUSELAGE 2023-106130<[01] REPLACED FWD DRAIN MAST IAW AMM 38-31-01-401-NG <BR>TEST IS OK <BR>TOOL USED P/N: 2278-20; S/N: AE-410983; DD: 06-JAN-24<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1:REPLACED Feb 3, 2023 · N566WN · Boeing 7377CTSDR AALA202302208528Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PREVIOUS REPAIR ANGLE OF KEEL BEAM AREA WING TO BODY AFT FAIRING FRAME LOCATED AT BS 727 AND BL 0. PREVIOUS REPAIR ANGLE #2 REMOVED AND FRAME REPAIRED PER EA 341801 AND SRM 51-40-02.Feb 2, 2023 · N903AN · Boeing 737823SDR AALA202302205228Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PREVIOUS REPAIR ANGLE OF KEEL BEAM AREA WING TO BODY AFT FAIRING FRAME LOCATED AT BS 727 AND BL 0. PREVIOUS REPAIR ANGLE #3 REMOVED AND REPAIRED FRAME PER EA 341801 AND SRM 51-40-02.Feb 2, 2023 · N903AN · Boeing 737823SDR AALA202302204860Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PREVIOUS REPAIR ANGLE OF KEEL BEAM AREA WING TO BODY AFT FAIRING FRAME LOCATED AT BS 727 AND BL 0. PREVIOUS REPAIR ANGLE #1 REMOVED AND FRAME REPAIRED PER EA 341801 AND SRM 51-40-02.Feb 2, 2023 · N903AN · Boeing 737823SDR SWAA2023031097264Panel · debondedPANEL 194BL FWD LOWER CORNER IS DISBONDED.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-60-70-0I-1 FIGURE 2; TABLE 2; ITEM [10] AND DWG DOC: 149A7558 ID: 0006<BR><BR>PANEL FWD LOWER CORNER IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PAR. 4.B.(6)<BR><BFeb 1, 2023 · N8524Z · Boeing 7378H4SDR SWAA2023031097261Panel · debondedPANEL 193AR OUTER SKIN IS DISBONDED NEAR I/B EDGE. (MARKED)<[01] IDENTIFIED MATERIAL OF PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 18; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.A(6)<BR><BR>ENGINEERIFeb 1, 2023 · N8524Z · Boeing 7378H4SDR SWAA2023020697347Doubler · crackedMULTIPLE CRACKS FOUND ON RH SIDE OF STA. 727 MLG BULKHEAD ANGLE DURING 193B PANEL INSPECTION. DETAILED CLEANING OF THE AREA IS REQUIRED FOR FURTHER INSPECTION TO DETERMINE EXTENT OF DAMAGED PARTS. MULTIPLE CRACKS FOUND ON RH SIDE OF STA. 727 MLG BULKHEAD ANGLEFeb 1, 2023 · N747SA · Boeing 7377H4SDR SWAA2023021696783Panel · corrodedCORROSION ON ACCESS PANEL 193B SUPPORT STRUCTURE AT BODY FAIRING 2023-83805<[01] TOOLS USED: POWER PACK P/N: PE1068; S/N: PE0118-94826; DUE DATE: 16-MAY-23; MULTIMETER P/N: FLUKE 87; S/N: 42180184; DUE DATE: 21-FEB-23; THERMOMETER P/N: 2278-20; S/N:AE-410983 ;Jan 31, 2023 · N276WN · Boeing 7377H4SDR SWAA2023013196148Panel · elongatedWING TO BODY FAIRING PANEL #193B HAS NUMEROUS ELONGATED HOLES.<[01] R&R PANEL 193B PER SRM 51-40-02-0G-0.Jan 28, 2023 · N445WN · Boeing 7377H4SDR SWAA2023030895861Panel · elongatedMID FORWARD BODY FAIRING PANEL #191D; ALL FASTENER HOLES ELONGATED OR/AND SURFACE PROTRUDING DOT 223-MFF191D.<[01] PERFORMED VISUAL INSPECTION ON PANEL #191D AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWATED MATERIAL PER B737 NDTM 51-05-01;[02] PREPAREDJan 26, 2023 · N567WN · Boeing 7377CTSDR R61A2023021500128Strap · corrodedAFT WING TO BODY FAIRING SUPPORT STRUCTURE HAS CORROSION BTWN STR 19R-STR 19L.MX REPLACED STRAPS IAW SRM 51-41-02Jan 25, 2023 · N208JQ · Emb ERJ170200LRSDR DALA2023012600667Subframe · worn(LOG 2597659) DURING INSPECTION FOUND LOWER WING TO BODY STRUCTURE FRAME STA 727+2.7 HAS MULTIPLE WEAR MARKS. REPAIRED FRAME PER DELTA ERA 605167-14AD REV. ORIGINAL.Jan 24, 2023 · N950DZ · Boeing 7379SDR SWAA2023021693621Fairing · pulled#3 FLAP TRACK FAIRING PANEL 542BB O/B SEAL RETAINER RIVETS PULLED THROUGH SIN. MRKD<[01] ACCOMPLISHED REPAIR TO AREA PER SRM 57-53-70-2R-2. SEE STEPS FOR INDIVIDUAL SIGNOFFS.;[02] SIGNED FOR PARTS.;[03] C/WJan 21, 2023 · N8610A · Boeing 7378H4SDR SWAA2023021393542Fairing · elongatedFOUND ELONGATED HOLES ON SUPPORT FAIRING 642BB MIDDLE SEAL SECTION R/H SIDE<[01] PREPARED FOR REPAIR FAIRING 642 BB; AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1.;[03] REPAIRED FAIRING 642BB AS PER B737 SRM 51-70-06-2R-9 MATERIAL USED PO.1800218 AND PO.1Jan 20, 2023 · N214WN · Boeing 7377H4SDR SWIA20230119Radome · damaged* RADOME HAS EVIDENCE OF COMPOSITE DAMAGE UNDER THE BOOT, AND AT THE 2, 4, & 8 O'CLOCK POSITIONS NEAR THE TRAILING EDGE, MARKED IN RED. (C-CHECK RO 2/23/2023) REMOVED AND REPLACED NOSE RADOME REF CRJ 900 AMM 53-81-80-400-801-A01 BONDING CHECK GOOD.Jan 19, 2023 · N827SK · Cndair CL6002D24SDR SWAA2023022306219Panel · peelingRIGHT SIDE OF FUSELAGE CENTER WING TO BODY FAIRING #193AR INNER SKIN FIBERGLASS PEELING OFF AT LOWER I/B EDGE<[01] CLEANED AND PREPARED AREA FOR REPAIR AT FUSELAGE CENTER WING TO BODY FAIRING 193AR AS PER BOEING 737 SRM 51-70-04-2R-6;[02] OK TO REPAIR DAMAGE AJan 18, 2023 · N213WN · Boeing 7377H4SDR SWAA2023022306218Panel · peelingLEFT SIDE OF FUSELAGE CENTER WING TO BODY FAIRING #193AL INNER SKIN FIBERGLASS PEELING OFF AT LOWER I/B EDGE<[01] PREPARED PANEL #193AL AT DAMAGED AREA FOR REPAIR PER B737 SRM 51-70-04-2R-6 AND SRM 51-70-04-2R-0;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] RJan 18, 2023 · N213WN · Boeing 7377H4SDR CALA2023012000154Door · bindingLAV DOOR 4L DIFFICULT TO OPEN FUP. ACCOMPLISHED ECRA INTERM REPAIR IAW ECRA 2549-01035. DIP APPROVED INTERIM REPAIR C/W 4L LAV DOOR LOWER BEAM BOX ASSY TOMC-APPROVAL FROM SC1ELBYC COMMENT ASSEMBLY AND GENERATE A DIP TO ACCOMPLISH PERMANENT REPAIR PER PART 3Jan 18, 2023 · N12004 · Boeing 78710SDR IPXA2023011990046Support Angle · crackedINSPECTION TYPE:C-1, RH UPPER WING TO BODY FAIRING ATTACH ANGLE CRACKED AT APPX. STA. 1239. REMOVED. FABBED AND INSTALLED RT WING TO BODY FAIRIHG SUPPORT ANGLE IAW SRM 51-31-01 AND DRAWING ANB7142Jan 18, 2023 · N270UP · Doug MD11FSDR SWAA2023020292027Panel · delaminatedDELAMINATED ACCESS PANEL 193AR UPPER SURFACE AT LOWER FUSELAGE 2023-37290<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18185847 DUE DATE: 24 SEP 23.;[03] TOOL USED SCALE P/N: SPX6Jan 16, 2023 · N215WN · Boeing 7377H4SDR SWAA2023011791633Panel · delaminatedBODY FAIRING PANEL 192 BL IS DELAMINATED AT FORWARD TOP EDGE AND MISSING 4 FASTNERS. R & R BODY FAIRING PANEL 192 BL IAW M/M 53-51-21.Jan 13, 2023 · N7844A · Boeing 737752SDR SWIA2023011001None · chafed*RH LOWER WING PLANK AT FS513.00 WS45.0 HAS CHAFFE DAMAGED FROM THE BODY FAIRING (MARKED) (C-CHECK RO 2/26/2023) BLENDED WITHIN LIMITS ZONE A (**), ORIGINAL MATERIAL THICKNESS 0.300", REMAINING 0.296", MATERIAL REMOVED 0.004"REF REO 601R-57-21-3692, RJan 11, 2023 · N466SW · Cndair CL6002B19SDR SWAA2023021489747Panel · crackedDELAMINATED ACCESS PANEL 194E AT LOWER FUSELAGE 2023-37819<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196126; DUE DATE: 24/FEB/23.;[03] TOOL USED SCALE P/N: 91847 S/N: AE-409322Jan 8, 2023 · N7825A · Boeing 7377CTSDR SWAA2023020289455Panel · crackedCRACK ACCESS PANEL 193AR HOLES AT LOWER FUSELAGE 2023-37045<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18185847 24 SEP 23.;[03] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196127Jan 7, 2023 · N215WN · Boeing 7377H4SDR SWAA2023021489039Panel · crackedCRACK ACCESS PANEL 192AL BODY FAIRING FASTENER HOLES AT LOWER FUSELAGE 2023-37724<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196126; DUE DATE: 24/FEB/23.;[03] TOOL USED SCALE P/Jan 6, 2023 · N7825A · Boeing 7377CTSDR SWAA2023021489041Panel · crackedCRACK ACCESS PANEL 192HL BODY FAIRING FASTENER HOLES AT LOWER FUSELAGE 2023-37716<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED SCALE PN: SPX621 SN: 8340225441 DUE DATE: 20/JUL/23.;[03] TOOL USED HOT BONDER PN: HCSJan 6, 2023 · N7825A · Boeing 7377CT
Back to JASC 5350