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 DALA2021081104603Skin · gougedSHIP 5646 WORKING PRI 593292-14 MTC DISCOVERED A GOUGE IN THE SECTION 48 FUSELAGE SKIN BETWEEN STRINGERS 19L AND 20L AND AFT OF FS 1787. CORRECTIVE ACTION: ALL WORK COMPLETED IAW ERA 593292-14 REV ORIG. (1902684)SDR DALA2021081004578Skin · gougedSHIP 5646 DURING EXT CLEANING EVENT 206 FOUND DENT AND GOUGE AFT LT SIDE JUST BELOW HORIZ STAB. CORRECTIVE ACTION: REMOVED DAMAGE IAW B757-200 SRM. C/W HFEC-NO CRACK. C/W BHEC OF REMOVED FASTENER HOLES - NO CRACKS PER B757 SRM. REPAIR INSTALLED PER ERA 593292-SDR DALA2022080405372None · noneDTE REQUIRED WITH 12 CALENDAR MONTHS PER ERA 593306-14. (FUSELAGE SKIN / #1, #5 LUG FITTING). LP# 1901680SDR R61A2021081400642Skin · corrodedAFT CARGO COMPARTMENT, CORROSION FOUND ON INTERNAL SIDE OF LOWER SKIN, BETWEEN FR 74-75 AND BETWEEN STR 28-29 RH. REPAIRED IAW ETD 170-025994SDR DALA2021081004585Skin · not reportedSHIP 193 DURING H CHECK MAINTENANCE FOUND UPPER SURFACE OF RT WING CTR SECTION STA 952 RBL 86-89. REPAIRED PER ERA 592436-14. (LP 7030796)SDR DALA2021081004574Skin · dentedSHIP 652 DENT ON FUSELAGE SKIN LOCATED STA 610, S-17LT. CORRECTIVE ACTION: SUMMARY OF NRC 01156: DENT ON FUSELAGE SKIN LOCATED STA 610, S-17LH WAS REPAIRED PER ETI-57-21-348 REV 9 AND ER/A 473252-14AD REV.B SECTION I: PERMANENT REPAIR #1. (1901479)SDR CALA2021080901290Skin · corrodedPOSSIBLE INTERIOR SKIN OR STRINGER CORROSION BETWEEN STA 360 TO STA 400 AROUND S-25 LEFT APPROX. [MARKED ON SKIN IN RED] FLEET CYCLE LOGPAGE #9781175. INITIATE A DTA DIP TO "ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS FROM AUGUST 2, 2021." NOTE TO PLANNING:SDR CALA2021080901288Skin · corrodedPOSSIBLE INTERIOR SKIN CORROSION NOTICED ON WASH, SKIN AND RIVETS BUCKLED FROM STA 360 TO STA 400 AROUND S-26 LEFT APPPROX. [EXTERIOR SKIN CIRCLED] FLEET CYCLE LOG PAGE 9780955. INITIATE A DTA DIP TO "ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS FROM JULY 29SDR SWAA2021091003811Bear Strap · crackedCRACK INDICATION FOUND AROUND FASTENERS ON BEAR STRAP (2EA) LOCATED BETWEEN BS 293 TO BS 293.5 AND BETWEEN STR 8 AND STR 9 RH SIDE IN FWD GALLEY AREA LENGTH (1) CRACK 0.260 INCH; LENGTH (2) CRACK IS 0 ; 2021-368567 / [01] TOOL USED P/N: NORTEC 500D; S/N: N500XSDR DALA2021080904542Skin · dentedSHIP 652 MONITOR INSP. REF. ER/A 473252-14AD REV. B; FUSELAGE SKIN DENTS AT STA 600 AND STA 640 BETWEEN S-16L AND S-18L. CORRECTIVE ACTION: REF ERA 473252-14AD. (1900518)SDR R61A2021080900620Skin · gougedGOUGE IN SKIN BETWEEN FR 21 AND FR22 AND STGR 14L AND 15L. REPAIRED IAW ETD2021-170-025518 REV CSDR R61A2021080500618Skin · dentedMAJOR-WHILE IN HEAVY CHECK - REAR FUSELAGE PROTRUDING DENT LH SIDE FR 96/97. REPAIRED IAW ETD2021-170-023889 REV B BY INSTALLING REPAIR DOUBLER.SDR DALA2024072407450Skin · discoveredSHIP 652 AN EXISTING REPAIR WAS FOUND ON FRAME 1640 BETWEEN STRINGER 16R AND 17R. ER/A 593222-14AD STA 1640 RH FOLLOW ON DAMAGE TOLERANCE ANALYSIS REQUIRED. CORRECTIVE ACTION: REF ERA 593222-14AD. (1899328)SDR DALA2021080604481Skin · corrodedSHIP 669 CORROSION ON FUSELAGE SKIN AROUND CUT OUT OF DOOR 119BL BTW STA 458 TO STA 460 AND BTW S-27L TO S-28L AT FUSELAGE (IN REF. NRC 00215). CORRECTIVE ACTION: SUMMARY OF NRC 00291; CORROSION ON FUSELAGE SKIN AROUND CUT OUT OF DOOR 119BL BTW STA 458 TO STA SDR CALA2021080601262Skin · corrodedUPPER FUSELAGE SKIN AT FR69-70 HAS CORROSION AROUND BONDING POIN TS AT STR2L AND 2R BS 69-BS70, STR 2L - STR 2R - A3NB-53-3-6208 - NR 9296419 (36419) GENERATED BY V077960 AT HAECO LCQ. ACCOMPLISHED INTERIM REPAIR AT FR 69-70 STR 1L - 2R IAW ECRA 534 1-01257 PASDR MASA20210804341Doubler · corrodedTCAS ANTENNA DOUBLER CORRODED. R&R TCAS ANTENNA DOUBLER IAW 51-42-06SDR EE4Y2021100313952Skin Panel · canningDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT FORWARD FUSELAGE SKIN PANEL WITH OIL CAN, LOCATED BETWEEN FR02 AND FR04, BETWEEN STRG-26L AND STRG-28R, THE DAMAGE
WAS REPAIRED INSTALLING AN EXTERNAL REPAIR DOUBLER AS PER E.O. # COO-EO-2021-13621 R00, ETD2021SDR SWAA2021091603287Doubler · damagedGROUND PWR DOOR CUTOUT FWD INNER DOUBLER HAS PIECE OF THE EDGE BROKEN BELOW LWR DOOR HINGE. 8-6 ; / [01] REMOVED EXTERNAL POWER DOOR #114AR TO GAIN ACCESS REF B737-700 SRM 51-40-02-0G-0.; [02] REMOVED EXTERNAL POWER RECEPTACLE BOX TO GAIN ACCESS REF B737-700 SSDR MASA20210810369Skin · corrodedCORROSION ON SETTLEMENT AREA OF AFT MAST DRAIN, BTW 27 TO 26RH AND FS:1031 TO FS:1047. SETTLEMENT AREA OF AFT MAST DRAIN, BTW 27 TO 26RH AND FS:1031 TO FS:1047 WAS REPAIRED PER EA 10-2021-036 REV A. AND DRAIN MAST SUPPORT CHANEL WAS REPLACED PER CRJ-900 SRM 5SDR HNAA2021081000383Skin · crackedE869171 - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTNERS FR 79 RH SIDE BELOW VERTICAL STAB. ... INSTALLED REPAIR BUSHING FOR (1 EACH ) ( MARKED ) ON FUSELAGE EXTERNAL SKIN AT FR 79 RH SIDE BELOW VERTICAL STAB IAW EMB 145 SRM 53-32-01, ITEM #9 AND EO1-53SDR HNAA2021081000382Skin · crackedE869173 - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 1 FASTNER FR 77 RH SIDE BELOW VERTICAL STAB ... REMOVED DAMAGE AT (1 EACH ) ( MARKED) FASTENER & INSTALLED REPAIR BUSHING FOR (1 EACH) ( MARKED) ON FUSELAGE EXTERNAL SKIN AT FR 77 RH SIDE BELOW VERTICAL STABSDR SWIA2021080960137Skin · scratchedSCRATCH /GOUGE IN LH LOGO NEAR MED (C-CHECK RO 8/5/2021) REMOVED DAMAGE BY BLENDING AND REMOVING DENT IAW BOMBARDIER REO 601R-51-00-309 REV -A DATED 2017-08-23 AND MHIRJ REO 601R-53-21-3476 REV -- DATED 2021-08-04. COMPLETED TASK CARD 51-900-1003-SKY ANSDR SWAA2021080900983Skin · cracked7' CRACK FROM FASTENER TO FASTENER AT RBL 54.0; JUST ABOVE HYDRAULIC SERVICE PUMP IN GFRP WEB MATERIAL. PERFORMED INTERIM REPAIR IAW SRM 57-10-10-1A-2 2.C. (3) (A). SPEED TAPE TO BE REINSPECTEDFOR CONDITION EVERY 600 FLT CYCLES. REF EA OTHER-57EA-03738.REF W/OSDR UIEA2021080601713Skin · corrodedCORROSION - FND 22EA CORROSION DAMAGE WHEN PERFORM SB 747-53A2878(<P>REMOVE THE ACCESS FASTENERS AND BLEND OUT CORROSION AREA IAW EI NO T2021A53M-2094 REV 0. REPAIR THE DAMAGED AREA IAW EI NO T2021A53M-2094 REV 2 AND SRM 51-40-02 REV 91 DWG NO 65B04124 SH15 RESDR UIEA2021080601730Skin · corrodedCORROSION DAMAGE ON INNER SURFACE OF FUSELAGE SKIN BETWEEN STA 1620 AND 1660, S-50L AND 51L(<P>REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 91. ACCOMPLISH EI T2021A53M-2152 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR MK1Y20210803005Skin · damagedDURING MAINTENENCE INSPECTION FOUND BLENDOUTS ON EXTERNAL FUSELAGE SKIN BETWEEN STA 1241 AND STA 1285, BETWEEEN STR 33L AND STR 34L, SEC 46.SDR MK1Y20210803004Skin · damagedDURING MAINTENENCE INSPECTION FOUND BLENDOUT AND SCRATCHES ON BULK CARGO DOOR CUTOUT, STA 1461, STR 27R - STR 31R.SDR MK1Y08032021003Butt Joint · damagedDURING MAINTENENCE INSPECTION FOUND BLENDOUT NEXT TO 3/16 HOLE AND BUTT JOINT, STA 12220, STR 33L - STR 34L.SDR MK1Y20210803002Skin · damagedDURING MAINTENENCE INSPECTION FOUND EXISTIG BLENDOUT ON FUSELAGE SKIN UNDER LAP SPLICE BETWEEN STA 266 AND STA 287, STR 17L.SDR MK1Y20210803001Skin · damagedDURING MAINTENENCE INSPECTION FOUND BLENDOUT AT EXTERNALFUSELAGE SKIN, AFT CARGO DOOR CUTOUT, STA 1350 - STA 1373, STR 20R - STR 25R.SDR DALA2021080404436Skin · dentedSHIP 652 INITIAL INSPECTION: SEVERAL DENTS ON SKIN FROM STA 1896 TO 1992 FROM S-1 TO S-10 LH (EVH). CORRECTIVE ACTION: SUMMARY OF NRC 1163. ALL DENTS ARE WITHIN LIMITS PER B757-200 SRM 53-80-01-1A, A.D. GENERAL, FIG 101, NOTE C, DETAIL IV. THE DENTS OUT OF LIMSDR CALA2021080201232Skin · crackedB767-06-3-0052 FUSELAGE EXTERNAL SKIN SURFACE 1EA FASTENER HOLE FOUND CRACK AT STA 1654.5 BTN S3R-S4R (AS MARK) REF NR LP 9130095 FUSELAGE EXTERNAL SKIN REPLACED AS PER EC/RA 5380-01290 REV - JUST AT STA 1654.5 BETWEEN STR-3R AND STR-8R THIS EC/RA PROVIDES ANDSDR FDEA202108011904Skin · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, MIDDLE FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND MIDDLE CRACKED FASTENER HOLE PER EA 6-SDR FDEA202108011903Skin · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, UPPER FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND UPPER CRACKED FASTENER HOLE PER EA 6-5SDR R61A2021080200615Skin · dentedAIRCRAFT HAS DENT ON FWD FUSELAGE AT FRA 9 TO FRA 11 AND AT STR 15L TO 18L. REPAIRED IAW ETD2021-170-024878 REV A ALSO REF VP-024228-2021 N/R #1.SDR DALA2021080204339Skin · dentedSHIP 3259 DENT EXTERNAL SKIN LOCATED BTW FR80 TO FR81 AT LEVEL STR4L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 593029-14 REV.0, PRI 593029-14 REV.1 AND ER/A 593029-14 REV. ORIGINAL. (1894892)SDR SWAA2021090700159Bear Strap · crackedFWD GALLEY DOOR (R1) BEAR STRAP HAS CRACK EMANATING FROM FASTENER HOLE OPPOSITE FITTING LATCH. ; / REPAIR AREA MAIN CABIN PER B737-700 AMM 20-60-07-913-801; [02] REMOVED RAIN GUTTERS FROM FWD AREA OF R1 DOOR CUT OUT BETWEEN S-9R AND S-10R AND AND RAIN GUTTER FSDR SWAA2021090712557Skin · dentedR/H FUSELAGE SKIN HAS A DENT AT STA: 1016+ 2.25'; BETWEEN S-17R AND S-18R; DENT MEASUREMENTS; L=5.125'; W=2.5'; Y=0.061'; W/Y=40.98 ; / [01] INSPECTED DENT ON R/H FUSELAGE SKIN; AT STA: 1016+2.25'; BETWEEN S-17R AND S-18R; DENT MEASUREMENT; L=5.125'; W=2.5'; YSDR HNAA2021083100405Skin · corrodedPOSSIBLE CORROSION BETWEEN SKIN AND STRINGER 18L CAUSING RIVET HEAD TO CRACK, DUE TO EXPANSION OF CORROSION. PERFORMED PERMANENT REPAIR OF FUSELAGE SKIN AT FR 61 AND STGR 18L IAW EO1-53-21-0204.SDR JJBA20210730017Doubler · corrodedCORROSION ON LOWER REAR FUSE 1, ON ANTENNA DOUBLER FOR AFT RADIO ALTIMETER #2 BTW FR 68-69. BTW FR 68-69, CORROSION FOUND ON LOWER REAR FUSELAGE 1. SUPPORT ANTENNA AND PLATE ASSEMBLY FOUND OUT OF LIMITS AND NEED TO BE REPLACED. SKIN BLENDED FOUND OUT OF LIMITSSDR SWAA2021091540221Skin · corrodedCORROSION ON FUSELAGE SKIN; AROUND FASTENERS; AT B.S. 907-947; B.L. 0; W.L. 306.5. ; / [01] INSTALLED EWIS/FOD PROTECTION UNDER AREA OF WORK BS 907-947 STR 1 PER AMM 20-60-07; [02] REMOVED FASTENERS BS 907-947 IN CROWN SKIN AT STR 1 FOR ACCESS PER SRM 51-40-02SDR A6WA202108097852Skin · corrodedFUSELAGE SKIN CORROSION AND SCRIBE MARKS AT VHF #1 ANTENNA LOCATION FS295.00 Ï¿½ FS310.00 S1L Ï¿½ S1R. AIRCRAFT REMOVED FROM SERVICE. BLENDED FUSELAGE SKIN CORROSION AND SCRIBE MARKS AT VHF #1 ANTENNA LOCATION FS295.00 Ï¿½ FS310.00 S1L Ï¿½ S1R. PERFORMEDSDR CALA2021073001215Skin · corrodedFUSELAGE SKIN CORRODED AND BULGED AT LAVATORY BLOWER PORT. ADDED PIC. PERFORMED STEP ON SRM 53-70-01-2R-3 PARA 4 STEP A THRU D COMPLETED STEP 4. (E), (G), (H), (I), AND (J). NO DAMAGE FOUND. REF: SRM 53-70-01-2R-3. STEP F VARIFIED MATERIAL PER SRM 53-70-01-2RSDR MASA20210729327Skin · damagedCENTER BAGGAGE BAY DOOR SORROUND STRUCTURE CLOSING SKIN WAS FOUND WITH 2EA. AREAS OF WEAR DAMAGE BETWEEN FS 629 - FS 661+16, STGR25L - STGR26. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 53-31-23-001-001-A02, ITEM 57B, EA 79-2021-195.
(PART/DEFECT LOCATIOSDR MASA20210729326Skin · dentedLOWER FUSELAGE SKIN PANEL BETWEEN FS280.00- FS295.00, STGR17R - STGR18R WAS FOUND TO HAVE 2 EA. DENTS. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 53-21-01-001-002-A01, ITEMS 1 AND E, EA 79-2021-197
(PART/DEFECT LOCATION: FS280.00-FS295.00, STGR17R - STGR18SDR MASA20210729321Skin · damagedLOWER FORWARD SKIN PANEL BETWEEN FS280-FS310 & STGR21L-STGR23L WAS FOUND TO HAVE PREVIOUS BLEND OUTS. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1, EA 72-2021-133.
(DEFECT PART/LOCATION: SKIN PANEL/FS280-FS310 & STGSDR MASA20210729318Skin · dentedFUSELAGE BELLY SKIN WAS FOUND WITH A DENT BETWEEN FS 250-FS 265 AND STR 23L -24L. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 55-21-01, FIGURE 53-11-01-991-808, ITEM 1, EA 69-2021-119.
(DEFECT LOCATION FS250-FS265 & STR23L-24L)SDR MASA20210729315Skin · damagedFUSELAGE SKIN BETWEEN FS333.00 & FS349.00 AND AT STGR 23 WAS FOUND TO HAVE A PREVIOUS BLEND OUT, THE BLEND TOOK PLACE OVER A FASTENER ROW. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 53-21-01, FIGURE 53-21-01-991-807, ITEM 1C, EA 83-2021-021.
(PART DEFECT SDR EE4Y2021072913438Skin · dentedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT CENTER FUSELAGE I UPPER SKIN PANEL, EXTERNAL SKIN WITH EXISTING REPAIR WITH DEVIATIONS LOCATED BETWEEN FR23 AND FR25, BETWEEN STR- 14L/17L, THE DAMAGE WAS REPAIRED INSTALLING A NEW EXTERNAL DOUBLER REPAIR AS PERSDR EE4Y2021072913436Skin · dentedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT CENTER FUSELAGE III LOWER SKIN PANEL, EXTERNAL SKIN WITH REWORK LOCATED BETWEEN FR83 AND FR84, BETWEEN STR- 23L/26L, THE DAMAGE WAS REPAIRED INSTALLING EXTERNAL DOUBLER REPAIR AS PER E.O. # COO-EO-2021-13202 R00
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