Boeing 737-33A
Service difficulty reports · 1,809
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 = '73733A' 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 aircraft_model_key = '73733A' 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 AWXA0002230Pressure Panel · crackedCOCKPIT FLOOR WEB CRACKED LBL 24, WL 207, BS 180. REMOVED AND REPLACED FLOOR WEB IAW ER 03-5311-01218-DD1.SDR AWXA0002218Doubler · crackedR1 DOOR LOWER AFT CORNER REPAIR DOUBLER FWD EDGE CRACKED .25 INCH AT TAPERED FILLER, FUSELAGE CUTOUT BS 318. REMOVED AND REPLACED TAPED FILLER PER SRM 53-10-01 PG 205 & 206.SDR AWXA0002244Web · crackedD: Crack LBL 4.8 WL 214 BS 178 Blkhd web Fwd side beneath strapC: Cutout damaged & installed doubler IAW B737-300 SRM 53-10-08 pgs 286-291SDR AWXA0002241Web · crackedD: Crack RBL 15, WL 221, BS 178 Blkhd web Fwd side beneath strapC: Cutout damaged area & installed doubler IAW B737-300 SRM 53-10-08 pg 291SDR AWXA0002231Web · crackedD: Cracks at 5 EA fastener holes BS 178 BLKHD web Fwd side, WL 234, RBL8,9,10,11,& 12C: Repaired damaged area IAW 737-300 SRM 53-10-08 pg 269-278SDR AWXA0002226Beam · corrodedD: Corrosion on top of floor beam BS 294 LBL 19C: Repaired floor beam IAW B737-300 SRM 53-10-51 pgs 220-223SDR AWXA0002196Web · crackedD: Crack RBL 1.5 WL 205 BS 178 Blkhd web fwd side beneath angleC: Cut out damaged area and installed doubler IAW B737-300 SRM 53-10-08 pgs 286-291SDR AWXA0002195Web · crackedD: Crack LBL 4.8 WL 214 BS 178 Blkhd web fwd side beneath strapC: cut-out damage & installed doubler IAW B757-300 SRM 53-10-08 pgs 286-291SDR AWXA0002189Web · crackedD: Cockpit floor web cracked LBL 24,WL 207,BS 180C: Removed and replaced floor web IAW ER 03-5311-01218-001SDR AWXA0002109Doubler · crackedD: R1 door lower aft corner repair doubler fwd edge cracked 1/4" at taper fuselage cut out BS 318C: removed and replaced tapered fillerSDR AWXA0002246Skin · corrodedFASTENER HEADS PULLING BS 947 STR 27 LT. CORROSION OUT OF LIMITS. INSTALLED REPAIR DOUBLER IAW ER 03-5361-01232-BA1.SDR AWXA0002220Floorbeam · corrodedCORROSION ON FLOORBEAM BS 986.5 RBL 18 TO LBL 18. REMOVED AND REPLACED T-CHORD IAW B737-300 SRM 53-60-51 PG 105-114.SDR AWXA0002193Skin · corrodedD: fastener head, pulling BS 947 STR 27LTC: Removed fastener, corrosion found. Removed corrosion, found to be out of limits installed repair doubler IAW ER 03-5361-01232-BA1SDR AWXA0002108Floorbeam · corrodedCORROSION ON FLOORBEAM BS 986.5 RBL 18 TO LBL 18. REMOVED AND REPLACED T-CHORD IAW B737 PER SRM 53-60-51 PGS 105-114.SDR AWXA0002242Bulkhead · crackedBLKHD 178 WEB FWD SIDE LBL 4.8 WL 193 AND 197 2 EA CRACKS EMANATING FROM BENEATH STRAP. CUT OUT DAMAGE, INSTALLED DOUBLER IAW B737-300 SRM 53-10-8 PG 287-291.SDR AWXA0002245Web · crackedD: BS 178 Blkhd web Fwd side RBL 4.8 WL 197 crack emanating from beneath strap.C: Cutout damaged area and installed doubler IAW B737-300 SRM 53-10-08 pgs 286-291SDR AWXA0002236Skin · corrodedD: Fastener heads pulling BS 967 STR 27RTC: Removed skin BS 908 to 1016 Removed corrosion, removal of material within limits, treat & primed and reinstalled skin IAW B737-300 SRM 51-40-02 pg 38 SRM 53-00-01 pg 104, SRM 51-20-01 pg 1 & SRM 51-40-02 pg 2 & 3SDR AWXA0002206Web · crackedD: BS 178 Blkhd web fwd side RBL 4.8 WL 197 crack emenating from beneath strap.C: Cut out damaged area and installed doubler IAW B737-300 SRM 53-10-08 pgs 286-291SDR AWXA0002219Skin · crackedNR 2 SLAT HAS CRACKS PROTRUDING FROM UNDER 2 RIVETS AT BOTTOM ROW UNDER O/B AUX ARM. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW B737-300 SRM 57-43-01 PG 216-219.SDR AWXA0002004Indicator · failedPHX -AIR TURNBACK- FLT 173- AFTER TAKEOFF FROM PHX THE NR 1 ENGINE EGT INDICATOR WENT TO ZERO AND THE AIRCRAFT RETURNED TO PHX. THE AIRCRAFT LANDED OVERWEIGHT AT 124.3 THOUSAND LBS AND 200 FPM SINK RATE. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED WITH NOSDR AWXA0002035Skin · damagedKEEL SKIN HAD 2 TEMPORARY REPAIRS STA 661 TO 726.5. REMOVED AND REPLACED SKIN PER AWA ER 03-5331-01193-SS1.SDR AWXA0002034Skin · dentedD: Fuselage skin at 1130 L/H STR 14L has 2ea dents in skinC: Fabricated and installed doubler repair per SRM 53-00-01SDR AWXA0002033Angle · corrodedD: Right crease beam corroded BS 294.5 to BS 345C: repaired per SRM 51-70-11 fig 1SDR AWXA0002031Skin · dentedDEEP DENT IN FUSE SKIN BS 1074 LBL 8. REPAIRED PER SRM 53-00-01 FIG 202.SDR AWXA0002025Clip · crackedD: BS 178 R/H clip is cracked at WL 209 RBL 27C: Removed and replaced clip per DWG 65-45883 and SRM 51-40-02SDR AWXA0002021Bulkhead · crackedFWD PRESSURE BULKHEAD BS178 CENTER WEB CRACKED RBL 5 & 7 WL 195 AND 210. REPAIRED PER SRM 83-10-08.SDR AWXA0002027Web · crackedD: BS 178 Bulkhead L/H intercostal web is cracked at WL 209 LBL 27C: removed damaged intercostal web installed new web IAw SRM 51-40-02 & DRW 65-45833SDR AWXA0002026Intercostal · crackedD: BS 178 L/H intercostal is cracked WL 195.7 LBL 27C: Removed and replaced intercostal IAW SRM 53-10-08SDR AWXA0002024Frame · crackedBS 178 LT SIDE CHORD IS CRACKED AT WL 204 LBL 27. REMOVED AND REPLACED SIDE CHORD PER SRM 51-10-2.SDR AWXA0002023Stiffener · crackedLBL 5.7 WL 182 VERTICAL CHORD IS CRACKED BS 178. ACCOMPLISHED REPAIR PER SRM 53-10-08.SDR AWXA0002022Intercostal · crackedD: BS 178 R/H intercostal cracked at WL 195.7 RBL 27C: Removed and replaced intercostal per SRM 53-10-08SDR AWXA0002029Floorbeam · damagedSTA 312 FLOORBEAM HAS NON SRM REPAIR. REPAIRED PER SRM 53-10-51.SDR AWXA0002030Floorbeam · corrodedD: STA 328 Floor beam Corroded from RBL 30 to RBL 45C: Repaired per SRM 53-10-51 Fig 205SDR AWXA0002028Floor Support · corrodedD: Floor support corroded STA 312 to 328 RBL 10C: Replaced support IAW 51-10-2 & 53-10-51SDR AWXA0002032Skin · damagedCREASE IN FUSELAGE SKIN BS 1120 LT STR 14L. REPAIRED PER SRM 53-00-01 FIG 202.SDR AWXA0001842Guard · out of positionPHX - AIR TURNBACK - 6/7/01 - FLT 519 - HEAVY ELEVATOR AFTER ROTATION; AIRCRAFT RETURNED TO AIRPORT W/ NO FURTHER PROBLEMS. MX FOUND CABLE PULLEY BRACKET AT STA 420 ON CABLE EBS WORN; REPLACED PULLEY BRACKET; AIRCRAFT RETURNED TO SERVICE. THE ELEV CABLE EB-5SDR AWXA0001837Pressure Panel · crackedleft main wheel well upper pressure web cracked at BS 664 LBL 33. repaired damaged area in web IAW ER 03-5702-01123-KB1.SDR AWXA0001836Intercostal · crackedaft side of BS 178 BLKHD RT intercostal is cracked WL 195 RBL 24. removed cracked intercostal; drilled, treated, primed and installed new intercostal IAW SRM 51-10-02 pg 15 and 51-40-02 pg 2&10.SDR AWXA0001835Intercostal · crackedvisual inspection of aft side of BS 178 BLKHD found LT intercostal cracked WL 195 LBL 24. removed and replaced cracked intercostal IAW SRM 51-10-02 pg 15 and 51-40-02 pg 2&10.SDR AWXA0001834Bulkhead · crackedHFEC indicates cracks at 4 HI-LOK fasteners in BS 178 BLKHD web WL 234.1 LBL 8-14. cut out damaged area and installed repair doubler and filler IAW SRM 53-10-08 pg 265-269 and 53-10-08 pg 265 item 13.SDR AWXA0001833Bulkhead · crackedHFEC indicates cracks at 4 HI-LOK fasteners in BS 178 BLKHD web WL 234.1 RBL 8-14. cut out damaged area of web and installed repair doubler and filler IAW SRM 53-10-08 pg 265-269.SDR AWXA0001832Skin · crackedaft cargo door skin cracked at lightening hole. cut out damaged area and installed repair doubler IAW SRM 51-70-13 pg 1 and 51-20-07 pg 215 and 51-20-01 pg 1.SDR AWXA0001831Skin · crackedleft wing NR 2 leading edge slat lower surface has 4 cracks from rivet holes. cut out damaged area and installed filler and repair doubler IAW SRM 57-43-01 fig 206.SDR AWXA0001830Frame · crackedfuselage frame inner chord cracked at FLOORBEAM attach point left side BS 616. cut out damaged area; FABBED repair angle and filler; drilled, treated, primed and installed repair IAW BOEING S/B 737-53-1182 and AWA ER 03-5311-01127-KB1.SDR AWXA0001829Frame · crackedvisual inspection of aft side of BS 178 BLKHD found LT side chord cracked WL 194-195 in center of radius. removed and replaced cracked side chord IAW SRM 51-10-02 pg 15 item NR 8 and 51-40-02 pg 2 & 10.SDR AWXA0001828Frame · crackedRT BS 178 chord cracked in center of radius WL 207. removed and replaced cracked side chord IAW SRM 51-10-02 pg 15 item NR 8 and 51-40-02 pg 2 & 10.SDR AWXA0001827Web · crackedaft side BLKHD vert web has 2 inch crack BS 183 WL 182.5. removed and replaced vert web IAW BAC DWG 65-17582 and SRM 51-40-02 pg 2, 3, 6, 7 and 38.SDR AWXA0001887Nut · looseIAH-AIR TURNBACK- INFLIGHT SHUTDOWN - FLT 831- DURING CLIMB THE NR 1 ENGINE EGT INDICATOR RED LIGHT ILLUMINATED. THE DIGITAL AND ANALOG EGT INDICATIONS SHOWED EXCESSIVE EGT. THE INDICATIONS WERE ERRATIC AND VARIED BETWEEN 700 AND OFF SCALE, OVER 1000. THE ESDR AWXA0001793Wedge · delaminatedLEFT WING INBOARD MID FLAP WEDGE PANEL DELAMINATED AT INBOARD BOTTOM SIDE. CUT OUT DISBONDED SKIN ON LWR SURFACE OF LT WING INBD MID FLAP WEDGE PANEL; MADE FILLER AND DOUBLER, ETCHED, TREATED AND PRIMED ADHESIVE PRIMER TO REPAIR AREA, BONDED REPAIR, TREATED SSDR AWXA0001792Wedge · delaminatedLEFT WING INBOARD MID FLAP WEDGE LWR SIDE HAS 2 AREAS OF DELAMINATION. REPAIRED IAW SRM 51-70-17 PG 68 & 70 AND AWA ER 03-5750-01145-JS1.
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