JASC 5330
Service difficulty reports · 79,347
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 SWIA201541434Skin · dentedSKIN HAS A DENT JUST AFT OF THE CAPT'S SIDE WINDOW. REPAIRED IAW SRM.SDR DALA2015091505664Skin · crackedSKIN HAS A .5" LONG CRACK, LATERAL AXIS, AT BS 1436.5. OTBD END OF CRACK IS 1.25" INBD OF L4R RIVET ROW. INSTALLED REPAIR IAW SRM 53-01, FIG 4, SHT 4.SDR DALA2015091505661Skin · dentedACFT ON RT FUSELAGE, SIGNIFICANT DENT 8.5" FORWARD AND 11.8" ABOVE THE ALTERNATE STATIC PORT CENTER. ALSO, THERE ARE 8 OTHER SMALL DENTS WITHIN THE CONTROLLED AREA 18", WHICH EXCEEDS THE MAXIMUM OF 2 DENTS, 1 SIDE IN THIS AREA. NR FOR ADDITIONAL INFORMATION 0SDR DALA2015091505659Skin · damagedACFT LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN LONGERON 1 AND LONGERON 2 RT BETWEEN BS 807 AND 826. LIGHTNING STRIKE WAS REPAIRED IAW SRM 53-04-2, PAR 3, FIG 2. SHEET 6.SDR DALA2015091505658Skin · damagedACFT AD INITIAL, LIGHTNING STRIKE ON RT FUSELAGE WINDOW BELT SKIN UPPER AFT CORNER BETWEEN BS 1231-1250. AREA WAS REPAIRED IAW ER/A 537761-14AD, REV ORIGINAL AND SRM 51-10-3, PAR 14, 21, AND SRM 51-30-5.SDR V0XD20150914191Skin · dentedDENT AT STATION 453.00 AT STRINGER 18R. REPAIRED DENT AT STATION 453.00 AT STRINGER 18R BY CUTTING OUT DAMAGE, FABRICATING & INSTALLING REPAIR PARTS IAW REO 670-53-21-1224 DATED 14 SEPT 2015 & REO 670-53-21-1224 REV P 1 DATED 10 SEPT 2015 & SRM 20-70-00. NDTSDR FDEA201509142858Skin · dentedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS AN EXISTING DENT AT BS 1380 - 1400, BETWEEN STRINGER 28 - 29. REPAIR CARRIED OUT IAW EA F-5330-T0320082 PART 1. CLASSIFIED AS MAJOR.SDR CALA2015091400755Skin · gougedDURING EXTERIOR CLEANING, FOUND ACFT SKIN TO BE GOUGED AT STATION 765, RBL 3. FABRICATED & INSTALLED REPAIR DOUBLER OF THE FUSELAGE SKIN AT STATION 765, RBL 3 IAW SRM 53-00-01 REPAIR 3 & SRM 51-40-0-2.SDR DALA2015100205938Skin · dentedON WALK AROUND FOUND DENT ON RK FWD FUSELAGE. BS 215. 7 O'CLOCK POSITION. 15" AFT OF RADOME BULKHEAD. REF ERA 539404-14, REV ORIG FOR REPAIR.SDR DALA2015092405864Skin · not reportedPERFORM PERMANENT REPAIR AROUND SAFETY JACK POINT EXTERNAL SKIN AT LOWER FUSELAGE FROM FRAME 73 TO FRAME 74 BETWEEN STR 32L TO STR 32R. IAW ER/A 506865-14, REV B, REF LOGS 0589859, 2134193, 2147703, 8836824.SDR SWAA2015092944376Skin · crackedFUSELAGE SKIN ON CRACKED AT BS 507, STRINGER 16R. REPAIRED SKIN IAW EA.SDR DALA2015091405613Skin · corrodedSKIN HAS AN AREA OF CORROSION, BS 578, STRINGER 29L. REPAIRED IAW SRM 53-04, FIG 12C, VIEW H.SDR DALA2016091209445Skin · damagedMTC REPORTED CORROSION, CRACKED SKIN, AND THREE PLUGS UNDER THE TCAS ANTENNA DOUBLER LOCATED BETWEEN FS 229-255 AND L-28L TO L-29R. ER/A 539193-14 WAS ISSUED TO REPAIR THE DAMAGE.SDR SWAA2015102145188Skin Panel · delaminatedKEEL BEAM EXTERNAL SKIN PANEL DELAMINATED AT BS 663.75, AT LOWER FUSELAGE. R & R PANEL IAW SRM.SDR SWAA2015100844710Bear Strap · crackedBEAR STRAP CRACKED BELOW EXTERNAL POWER DOOR LOWER HINGE. REPAIRED BEAR STRAP IAW EA & ER.SDR SIMA20150912004Skin · crackedLEFT UPPER FUSELAGE SKIN HAS 2 CRACKS AT FRAME 75 & ABOVE STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1676.SDR SIMA20150912006Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN IAW ERS-EM-53MR-1675.SDR SWAA2015100144421Skin · delaminatedTAIL CONE FUSELAGE EXTERNAL SKIN DELAMINATED AT BS 1156+10, LBL 8. REPAIRED SKIN IAW SRM.SDR 7C7A20150930088Skin · dentedDENT ON LT FUSELAGE AT STATION 357, BETWEEN STRINGER 31 - 32. REPAIRED WITH DHC-8 SRM 53-30-21, WP479 & WC1014.SDR SWAA2015092144114Skin · crackedSKIN CRACKED AT BS 294, BL0. REPAIRED SKIN IAW EA.SDR SWAA2015091743989Skin · crackedSKIN CRACKED AT BS 520+7, STRINGER 28L. REPAIRED SKIN IAW EA.SDR DALA2015091205648Skin · crackedDURING LINE CHECK, MAINTENANCE NOTED A SKIN CRACK ON THE RT FUSELAGE AT BS 1076, STR 14 RT. THE CRACK WAS APPROXIMATELY 1.4" IN LENGTH. REPAIRED IAW ER/A 539301-14.SDR DALA2015091305643Skin · wornWEAR ON STRIP LT/RT FORWARD SIDE LOWER SKIN AT AFT ACCESSORY COMPARTMENT. DAMAGE REMOVED. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-00-01, FIG 6 AND 51-30-20.SDR DALA2015091405616Skin · corrodedBELLY SKIN BULGED, FASTENERS PULLED THROUGH BS 555 STRINGER 29R. REPAIRED IAW SRM 53-04, FIG 12C.SDR DALA1703243714Skin · crackedBS 540 SKIN CRACKED, REPAIRED IAW AA 5331-01257SDR SWAA2015092144096Skin · crackedFUSELAGE SKIN CRACKED AT BS 360, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.SDR SWAA2015091743977Skin · crackedSKIN CRACKED AT BS 520+3, STRINGER 6L. REPAIRED SKIN IAW SRM.SDR DALA2015091205640Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BS 427-434 BETWEEN LONGERON 29-30R. EXCESSIVE DAMAGE. REPAIRED IAW SRM 53-30-02, 51-30-02, 51-10-03.SDR SIMA20150910007Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2R ON FRAME 75, APPROX 1/2" LONG. REPAIRED RT UPPER FUSELAGE SKIN AT 1ST FASTENER BELOW STRINGER 2R ON FRAME 75 IAW ERS-EM-53MR-1688.SDR SIMA20150910006Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R, APPROX 3/8" LONG. CRACK ON RT REAR FUSELAGE 1 EXTERNAL SKIN AFT OF FRAME 75 ABOVE STRINGER 2R WILL BE CUT OUT & REPAIRED WITH FILLER & DOUBLER, SEE NRTC E471752 FOR CORRECTIVE ACTION.SDR SIMA20150910004Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED AT 1ST FASTENER BELOW STRINGER 2L ON FRAME 75, APPROX 3/8" LONG. EASI 8071 USED, 100-500 KHZ PROBE, FREQ=400, V-GAIN=78.5, H-GAIN= 65.0, LPF=100. REPAIRED LT UPPER FUSELAGE SKIN AT FIRST FASTENER BELOW STRINGER 2L ON FRAME 75SDR AALA20150913001Skin · chafedLEFT FWD FUSELAGE SKIN CHAFING MARK FOUND, BETWEEN STATION 254.5 - 265.5, STRINGER 34L AREA. LT FWD FUSELAGE SKIN REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 202 REPAIR 13.SDR 39LA20150910144Access Panel · missingDURING POST FLIGHT INSPECTION, THE FLIGHT CREW DISCOVERED THAT THE LT SIDE TRANSMISSION MX PANEL WAS MISSING. REPLACED PANEL, REMOVED FROM THAT WAS INSPECTED & FOUND TO BE IN A SERVICEABLE CONDITION, THE PANEL WAS REPLACED IAW S-61MM CH 53-30-0. PANEL PN S61SDR V0XR2015091000002Skin · corrodedCORROSION FOUND ON THE INTERIOR SURFACE OF THE FUSELAGE SKIN BETWEEN FRAMES 12-13 AND STRINGERS 2021R. REPAIRED IAW ETD-2015-145-070110, REV C, REPAIR B AND EO-EMB145-53-013-R2.SDR CALA2015091194294Skin · damagedREF ECRA 5310-06591, REPAIR AT STATION 1197+66, STRINGER 1 - 4, 12 HOLES ELONGATED. REPAIR WAS ACCOMPLISHED ON NR 23045 IAW ECRA STEP 4. CF STATING THIS REPAIR IS FIRST STAGE APPROVAL ONLY. THIS REPAIR MUST BE REPLACED WITHIN 12 MONTHS, UNLESS APPROVAL FORMSDR V0XR2015091000001Skin · corrodedCORROSION AND PIN HOLES IN SKIN AT FR 13-14, STR 16-17R. REPAIRED CORROSION DAMAGE BY CUTTING THE SKIN BETWEEN FRAME 13-14, STR 16-17R AND INSTALLING A NEW SKIN SECTION AND DOUBLER, TRIPLE IAW ETD2015-145-07011 AND EO EMB145-53-013 R2. THIS REPAIR IS CONSIDESDR 7C7A20150907081Skin · dentedDENT ON LT FUSELAGE SKIN AT STATION X226, BETWEEN STRINGER 25P - 26P.SDR 7C7A20150907078Skin Panel · dentedDENT ON LT FUSELAGE SKIN AT STATION X226, BETWEEN STRINGER 25P - 26P.SDR GLBA2015091000535Skin · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND BELLY CORROSION AT FS 243.25 & STRINGER 15L. REPAIRED IAW EO 15-1900-52-012.SDR CALA2015091000740Skin · damagedMEASURED DENT AT STATION 1580, ABOVE STRINGER 20L & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 PG 104 ALLOWABLE DAMAGE 1 DETAIL III. DENT IS CLOSER THAN .5 INCHES FROM FRAME AT STATION 1580. WORK WITH LP 5889353, JOB 112 CUT OUT DAMAGED AREA OF FUSELAGE SKINSDR CA151006007Paint · peeling(CAN) THE FIRE PROTECTION PAINT USED ON THE FUSELAGE BELLY AND ENGINE COWLINGS IS PEELING. INVESTIGATION UNDERWAY AS TO CAUSE OF THE PEELING. THE MANUFACTURER IS DISPATCHING A PAINT TECHNICIAN TO CARRY OUT REPAIRS AND ASSIST IN OCCURRENCE INVESTIGATION.SDR DALA2015091005635Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN, BS 178, BETWEEN STRINGERS 28 - 29L. REPAIRED IAW SRM 53-31-02, PARA 3C.SDR DALA2015091005587Skin · corrodedDURING INSPECTION, FOUND LOWER EXTERNAL FUSELAGE SKIN LT SIDE BS 1016, STRINGERS 20 - 27L SKIN CORRODED AT BUTT JOINT. MAINTENANCE REPAIRED THE SKIN IAW PRI 537900-14, REV 0 AND ER/A 537900-14, REV ORIGINAL.SDR DALA2015091005572Skin · damagedEVIDENCE OF DAMAGE TO LOWER FWD SKIN BETWEEN FRAMES 25-26 AND STRINGERS 44-43R PRI/ERA ISSUED 539169-14 REV 0 REV 1 REV 2 REV 3. C/W PRI/ERA 539169-14 REV 0,1,2 AND 3.SDR CALA2015091194291Skin · dentedDENT IN THE FUSELAGE SKIN & DOUBLER AT LOWER AFT CORNER OF FWD CARGO DOOR CUT OUT AT BS 613 ABOVE STRINGER 26R. REPAIR ACCOMPLISHED ON ECRA 5331-01783.SDR 7C7A20150907076Skin · dentedFUSELAGE DENT DAMAGE, STATION X291.4, BETWEEN STRINGER 29S - 30S.SDR AALA20150908015Skin · dentedDENT IN AFT CARGO DOOR CUT OUT STRUCTURE, LOWER AFT AREA. INSTALLED FILLER, DOUBLER & TRIPLER IAW SRM 53-00-1-2R-24, 51-20-02 & EA 254379A DATED 9 10 15.SDR DALA2015090905597Skin · dentedDENT ON FUSELAGE SKIN, BS 223 BETWEEN LONGERONS 17 - 18L. REPAIRED IAW SRM 53-30-01, 51-30-02, 51-30-05 AND 51-10-03.SDR DALA2015090905496Skin · damagedACFT HAD LIGHTNING STRIKE FUSELAGE BS 400 LONGERONS 1-2R. LONGERON AND SKIN WAS REPAIRED WITH PERMANENT REPAIR IAW SRM 53-04-2, FIG 2, SHEET 26 AND 53-02, FIG 18.SDR SWAA2015092544278Skin · crackedSKIN CRACKED AT BS 806-2, STRINGER 19L. REPAIRED SKIN IAW EA.
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