JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 jasc_code = '5330' 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 DALA2024080707853Skin · crackedCRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW CUTOUT AREA WAS FOUND. SUMMARY OF NRC 00628: INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1 PARAGRAPH 5 FIGURE 201.SDR DALA2024080607841Skin · crackedCRACKS ON FUSELAGE SKIN LH SIDE BTW LONGERON 13L-14L AND STA 1022, 1037, 1087 AT AFT FUSELAGE. SUMMARY OF NRC 00046: (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FUSELAGE SKIN LH SIDE BTW LONGERON 13L-14L AND STA 1037, 1087 AT AFT FUSELAGE ON STA 1037 THREE CRACKSSDR 2024FA0000569Skin · dentedREWPAIR - SECTION 41 - DENT - RH FUSELAGE SKIN BETWEEN STA 303 AND 325 AND BETWEEN STR 35R-36R.SDR HNAA2024091200787Skin · cracked53-2033 CRACK AT RH RF1 FR75 BTW STR2-3R. REPAIRED IAW EO1-53-24-0516SDR R61A2024082900372Skin · dented***MAJOR*** REF DMI R1216513/2 UPPER SKIN BTWN FR11-12 STR05L-06L DENTED. MX REPAIRED DENT IAW ETD2024-018166.SDR R61A2024082900370Skin · dented***MAJOR*** DENT FOUND FWD OF L1 DOOR. MX REPAIRED IAW ETD 2024-018166 ---MAJOR***SDR SIMA20240805003Skin · dentedREF ITEM1 BIRD STRIKE FOUND DENT RH SIDE OF NOSE FRAME 5 STRINGER 10 2.25IN X .25 IN MAJOR REPAIR. TRANSFERRED FROM AML PAGE 5167174 ITEM 2. J. WILLIAMS 507866. PERFORMED DOUBLER TRIPLER PATCH MAJOR REPAIR ON BIRD STRIKE SKIN DENT AT FR 5 STR 10 IAW ERS-EJ-53MSDR DALA2024080807876Skin · unknownSHIP 3275 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC BTW FR33 TO FR34 AND BTW STR41L TO STR41R LOWER FUSELAGE ( REFERENCE DOC. AA CARD 5100-01821-01A). C/A: CONFIRMED DT EVALUATION FOR FCS REPAIR ON LOC BTW FR33 TO FR34 AND BTW STR41SDR DALA2024080807875Skin · unknownSHIP 3275 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC BTW FR74 TO FR75 AND BTW STR23R TO STR24R LOWER FUSELAGE ( REFERENCE DOC. AA CARD 5100-01821-01A). C/A:CONFIRMED DT EVALUATION FOR FCS REPAIR ON LOC BTW FR74 TO FR75 AND BTW STR23RSDR DALA2024080707870Skin · gougedSHIP 5656 **DTE REQUIRED**, ERA 619917-14, STA 640 / STR18L & STR 20L / DENT AND GOUGES MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME AT STA 640 BETWEEN S-18L & S-20L. CORRECTIVE ACTION: REF ERA 619917-14. (0486260)SDR YENA2024080601090Skin · puncturedDURING HEAVY MAINTENANCE: UPPER FUSELAGE, ON FR80 BETWEEN STGR 2RH AND STGR 3RH WITH A PUNCTURE; UPPER FUSELAGE, ON FR80 BETWEEN STGR 2RH AND STGR 3RH PUNCTURE WAS REPAIRED, THIS REPAIR IS CAT A, NO REQUIRES FURTHER ACTION I.A.W SRM 53-51-- 11-300-002 REV 149 SDR DALA2024080507751Skin · ground damageSHIP 3410 DURING BOARDING AC CAME INTO CONTACT WITH WORK STAND JUST BELOW BULK CARGO DOOR. CORRECTIVE ACTION: REPAIRED PER ERA 619702-14, CONTINUE TO MONITOR. (0484914)SDR DALA2024080707846Skin · damagedSHIP 3275 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC BTW FR 69 TO FR70 AND BTW STR29R TO STR32R LOWER FUSELAGE (REFERENCE DOC. AA CARD 5100-01821-01A). C/A: CONFIRMED DT EVALUATION FOR FCS REPAIR ON LOC BTW FR69 TO FR70 AND BTW STR29SDR DALA2024080507754Skin · ground damageSHIP 3410 SKIN BETWEEN FR68 - FR69 AND STGR49RH / GROUND IMPACT DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 619702-14 SECTION II (0484515)SDR CALA2024080502160Skin · damagedFOUND A LIGHTENING STRIKE NICK ON LOWER FUSELAGE FWD OF AFT E&E DOOR NEXT TO T-CAS LEFT SIDE SEE PICTURES. REPAIRED LOWER SKIN AND E&E DOOR CHORD AT STA 310 LBL 6.7 PER ECRA 5311-03256 ESFR CREATED DIPS ON LOG 8831186 AND 8831255 ALSO REF BAM N/R 2103642 THISSDR SWAA2024090622303Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL AT LOWER FUSELAGE 2024-473211<[01] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE:07-NOV-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25/JAN/25;[03] TOOL USED: SCALE: P/N:CR5200 S/N:8343110809 DUSDR CALA2024082202250Skin · damagedDURING AAI UNABLE TO LOCATE EXTERNAL FUSELAGE REPAIR DOUBLER RECORDS AT LEFT OF THE NOSE WHEEL WELL EXTERNAL SKIN APPROX. FRAME 18 BETWEEN STR 34L AND 37L JUST ABOVE LEFT SIDE OF THE AIRCRAFT NOSE NUMBER. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATESTSDR SWIA2024081203Skin · dentedADM # N507SY-8548 DENT IN UPPER FWD FUSELAGE SKIN BETWEEN FR 8 AND FR 7 BELOW STRGR 15R. PLEASE EVALUATE DENT AND CORRECT AS NECESSARY. (C-CHECK RO 8/10/2024) PERFORMED PERMANENT DOUBLER REPAIR ON RH FWD FUSELAGE SKIN FR 7-8 STGR 15R-17R REF. SRM 53-10SDR VNAA202408090003Skin · damagedFUSELAGE LOWER SKIN BTWN STRG 25L - 26R BTWN FS280.00 - FS333. REPAIRED PER REO 690-53-21-1804 REV. --SDR VNAA202408080004Skin · dentedDENTS TO FUSELAGE SKIN BETWEEN FS193.00 - FS202.75. FUSELAGE SKIN BETWEEN FS193.00 - FS202.75 WAS REPLACED PER REO 690-53-11-1812 REV.-- AND CRJ-900 SRM 51-42-06-001-001-A01SDR IXXA202408030004Skin · crackedFUSELAGE SKIN AND BEAR STRAP IS CRACKED SINGLE FASTENER HOLE AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT STA 335 JUST ABOVE S20R. (VERIFIED WITH HFEC HOLE SCAN)SDR IXXA20240803004Skin · crackedFUSELAGE SKIN AND BEAR STRAP IS CRACKED SINGLE FASTENER HOLE AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT STA 335 JUST ABOVE S20R. (VERIFIED WITH HFEC HOLE SCAN)SDR SWAA2024090621613Panel · debondedPANEL 195BR OUTER SKIN IS DISBONDED NEAR AFT END. (MARKED)<[01] 195BR OUTER SKIN DISBOND DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR IPXA2024082266971Skin · gougedCREW DOOR CUTOUT, AFT MID AREA WITH GOUGE. GIVEN OK TO RESTORE PROTECTIVE COATINGS. RESTORED PROTECTIVE COATING PER SRM 51-21-10.SDR DALA2024080507763Skin · crackedCRACKS ON FUSELAGE SKIN RH SIDE BTW LONGERON 13R-14R AND STA 1116, 1144, LONGERON 7R AND STA 1022 AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN RH SIDE BTW LONGERON 13R-14R AND STA 1116, 1144, LONGERON 7R AND STA 1022 AT AFT FUSELAGE WAS REPAIRED PER PRSDR IXXA2024080201Skin · crackedAFT CORNOR OF L1 DOOR CUTOUT THE SKIN IS CRACKED AT THE LOWER FASTNER HOLE STA 335 JUST ABOVE FLOOR LEVEL (FOUND WITH HFEC OPEN HOLE SCAN)SDR SWIA2025010600801Skin · dentedCOMPLY WITH REPAIR AUTHORIZATION: RA90819-REO601R-53-11-3928 MXCODEID74488-PR - CW REO 601R-53-11-3928 TEMPORARY DISPOSITION TO FUSELAGE SKIN DENT BTWN FS220.00 - FS235.00 AND BTWN STRINGER 12L AND PILOT SIDE WINDOW LOWER SILL. PERMANENT REPAIR IS DUE WITH IN SDR SWIA202501030002Skin · dentedCOMPLY WITH REPAIR AUTHORIZATION: RA90819-REO601R-53-11-3928 MXCODEID74488-PR - CW REO 601R-53-11-3928 TEMPORARY DISPOSITION TO FUSELAGE SKIN DENT BTWN FS220.00 - FS235.00 AND BTWN STRINGER 12L AND PILOT SIDE WINDOW LOWER SILL. PERMANENT REPAIR IS DUE WITH IN SDR HNAA2024091200784Skin · gouged53-2015 GOUGE ON EXTERNAL SKIN AT FR68 BTW STR15-16L. REPAIRED IAW EO1-53-24-0520SDR YENA2024080601081Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOC.FR13 TO FR14 AND 3.500 INCH LOWER OF LH SIDE ST R AT LOWER FUSELAGE; (RESOLVED ON W/O: 1275940 TASKCARD: NR-00004) REF AEROMAN WO 2024 208/1 WCC 2024-337448 EVALUATED DENT LOC. ON EXTERNAL SKIN LOC.FR13 TO FR14 SDR YENA2024080601080Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN BTW FR 27 TO FR 28 AND BTW STR 30L TO STR 31L AT L OWER FUSELAGE;(RESOLVED ON W/O: 1275940 TASKCARD: NR-00005) REF AEROMAN WO 2024 208/1 WCC 2024-337624 EVALUATED DENT AND FOUND WITHIN NEGLIGIBLE LIMITS I.A.W A320 SSDR YENA2024080601074Skin · corrodedREPORTED MULTIPLE (7) SPOTS OF CORROSION ON THE INNER SKIN OF THE FWD FUSELAGE BETWEEN FR 33-34 & STR 41L-40R IN THE FWD CARGO COMPARTMENT. THE CORROSION WAS REMOVED BY BLEND OUT, BUT FOUND TO BE OUT OF LIMITS OF A320 SRM TASK 53-21-11-283-018 DUE TO THEIR LOSDR VNAA202409020010Skin · dentedDURING DETAILED VISUAL INSPECTION OF THE FUSELAGE SKIN IN REFERENCE TO JOB CARD TRFKE0080LHU/// DENT ON FUSELAGE SKIN FS 394.00 BLWN STGR 19 LH AND 20LH. DENT ON FUSELAGE SKIN FS 394.00 BLWN STGR 19 LH AND 20LH WAS REPAIRED PER REO 690-53-21-1823 REV--SDR CALA2024080602163Skin · corrodedREPAIRED CORROSION ON INTERNAL SKIN DOUBLER AT CUTOUT FOR PANEL 154AR IAW UNITED EC/RA 5300-03134 AND AMES DOC #47625REA02. REPAIRED CORROSION ON INTERNAL SKIN DOUBLER AT CUTOUT FOR PANEL 154AR IAW UNITED EC/RA 5300-03134 AND AMES DOC 47625REA02. SEE PARTIAL SDR DALA2024080107699Skin · dentedSHIP 3170 DENT IN THE FUSELAGE SKIN FWD OF L1 DOOR LOWER FWD CORNER BETWEEN FR12- FR13 AND STR 24L- STR 25L. CORRECTIVE ACTION: REPAIRED PER PRI 619782-14. (0476771)SDR DALA2024080107683Skin · gouged(LOG 0476998) FUSELAGE SECTION 48 SKIN BS 1088-1156 S-4R & S-6R GOUGE. REPAIRED PER ERA 619788-14.SDR IXXA20240731013Bear Strap · corrodedCORROSION ON THE BEAR STRAP, FWD OF FRAME 1562, BETWEEN STR.39L AND STR.39RSDR IXXA2024073109Skin · crackedLOWER AFT CORNER OF R1 DOOR CUTOUT THE SKIN IS CRACKED @ 2 LOWER FASTENER HOLESSDR 2024F00181Door Frame · crackedUPPER LEFT CORNER AFT PACK NO.3 ACCESS 114AR VISUAL CRACK FOUND APPROX. .75 IN PICS ATTACHED. VERIFIED ALL INSP STEPS COMPLIED WITH ON EO-90589-PRELIM1 RIGHT-SIDE AIR-CONDITIONING DOOR JAMB CORNER SKIN CRACK- PRELIMINARY REPAIR NO. 1SDR IPXA2024073196756Skin · damagedIMPACT DAMAGE BY CONTAINER ON FUSELAGE SKIN STA. 1340 STRINGER 25L REMOVED 4 RIVETS AT S25L AND REMOVED 6 RIVETS AT STA 1340 BETWEEN S25L AND S26L.REMOVED 4 RIVETS AT S25L AND REMOVED 6 RIVETS AT STA 1340 BETWEEN S25L AND S26L.PERFORMED MATERIAL REMAINING DAMASDR SWAA2024090319504Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 500D BTW STR 18L TO STR 19L AT BODY FAIRING STRUCTURE 2024-458810<[01] REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS 500D BTW STR 18L TO STR 19L AT BODY FAIRING STRUCTURE . IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM SDR AALA202408122646Skin · bulgedAIRCRAFT IN BASE MAINTENANCE: BULGE IN FUSELAGE SKIN AT STA 727J, S14R. REPAIRED SKIN PER EA 356413.SDR CALA2024080702177Skin · damagedDURING ACCOMPLISHMENT NR 2114213 WAS FOUND A DAMAGE ON FUSELAGE SKIN LH SIDE BETWEEN STA 1702 AND 1746.125 , STRINGER 24L AND 26L. ITS NECESSARY TAKE ACTION TO PERFORM A REPAIR IAW SRM. TO PERFORM INSPECTION IAW SRM 53-00-01-2R-12 TABLE 202 & DELIVERY, REPEATSDR SWAA2024080518605Skin · crackedR1 DOOR FWD CUTOUT PANEL CRACKED AT LOWER SECTION<[01] REPAIRED R1 DOOR FWD CUTOUT PANEL AT LOWER SECTION AS PER B737 AMM 25-00-00-300-802.;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02SDR DALA2024073007635Skin · puncturedAIRCRAFT 3066, WHILE IN DTW, SUBJECT AIRCRAFT SETTLED ON A STATIONARY LADDER SUSTAINING GROUND DAMAGE. THE DAMAGE CONSISTS OF A DENT WITH PUNCTURE THROUGH THE NOSE FORWARD FUSELAGE SKIN (P/N: D5313708920000) JUST OUTBOARD OF THE E&E BAY ACCESS DOOR. THE DENTEDSDR AALA202407301964Exhaust Port · corrodedAIRCRAFT WAS GROUNDED: WASTE TASK EXHAUST PORT HAS SIGN OF CORROSION AROUND. INSPECTED AREA AND PERFORMED REPAIR AT WASTE TANK EXHAUST PORT. PER AMM 38-32-00-140-801.SDR R61A2024073000343Skin · dentedLH FWD FUSELAGE SKIN HAS DENT WITH CREASE LOCATED AT FRAME 11 TO FRAME 12 AND STR 5L TO 6L. REPAIRED DENT IAW ETD2024-170-020454, ALSO REF VP-028165-2024 N/R #2 FOR WORK ACCOMPLISHED.SDR R61A2024080900346Finger Doubler · corrodedFORWARD CARGO DOOR CUTOUT AFT FINGER PLATE IS CORRODED FR 26-27. REMOVED AND REPLACED FWD CARGO DOOR CUTOUT, AFT FINGER DOUBLER REF. SRM 51-40-08.SDR DALA2024073007613Panel · dented(LOG 0469485) DENT 4FT FWD OF LAV SVC PANEL. REPAIR PER B737-900 SRM 53-00-01-2R-36.SDR DALA2024072907584Skin · dented(LOG 0469448) DENT 4FT FWD OF LAV SVC PANEL. COMPLETED REPAIR PER B737-900 SRM 53-00-01-2R-36.
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