Boeing 737-277
Service difficulty reports · 1,584
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 = '737277' 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 = '737277' 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 AWXA0002087Seat Track · nickedD: Seat track RBL 45-50 STA 360-947 is nicked @ various locations.C: Track blended and protected per SRM 53-10-1 pg 18. STA 520-540 track replaced per SRM 51-30-2 Pg * STA 827 track repaired per SRM 53-10-5 pg 3, and SRM 51-30-2 PG 8SDR AWXA0002051Stiffener · crackedD: Pressure web stiffener cracked at BS 727, LBL 17, WL 202C: Removed and replaced stiffener IAW B737 SRM 51-30-2 Pg 8SDR AWXA0002086Stringer · corrodedD: S-26L STA 727-727A +10 corroded beyond limits.C: S-26L STA 727-727A +10 repaired per SRM 53-10-3 Fig 1 pg 2 and SRM 51-30-2 pg 2 & 8SDR AWXA0002085Seat Track · nickedD: Various nicks found along seat track LBL 45-50 STA 360-947C: Nicks dressed and assessed per SRM 51-10-1 Pg 18 STA 540-564 track repaired per SRM 53-10-5 Fig 2 Pg 2-5SDR AWXA0002134Stiffener · crackedD: Pressure web stiffener cracked BS 727 LBL 8 WL 202C: Removed and replaced pressure web stiffener IAw B737 SRM 51-30-2 pg 8SDR AWXA0002133Angle · corrodedT-ANGLE FWD SIDE OF BS 1088 BULKHEAD CORRODED AT RBL 33 WL 228 TO 240. REMOVED AND REPLACED T-ANGLE IAW B737 SRM 51-30-2 PG 2&3.SDR AWXA0002132Stiffener · corrodedD: Stiffener on FWD side of BS 1088 Bulkhead corroded at RBL 27 WL 240 to 228C: Removed and replaced stiffener IAW B737 SRM 51-30-2 pg 2&3SDR AWXA0002130Angle · corrodedLEFT ANGLE ON BS 1088 BULKHEAD CORRODED AT WL 243 RBL 23 TO RBL 32. REMOVED AND REPLACED LEFT ANGLE IAW B737 SRM 51-30-2.SDR AWXA0002128Firewall · damagedE1 HYDRAULIC PRESSURE LINE AT TRANSITION THOUGH PYLON, LOOSE; NR 1PYLON. REPAIRED NR 1 ENG FIRE WALL PYLON IAW ER 15-5412-01202-DL1.SDR AWXA0002041Frame · gougedD: Previously repaired gouge at BS 480 frame BL-0 requires reworkC: Removed old repair and repaired frame IAW AWA ER #15-5332-01204-TB1SDR AWXA0002040Frame · corrodedD: Verify material type of repair at BS 480 frame, STR 24R at Aft cutout of fwd cargo doorC: Removed existing repair and replaced IAW AWA ER 15-5332-01204-JS1SDR AWXA0002011Web · crackedD: HFEC Indicates 1.7" crack BS 178 BLKHD pressure Web, LBL .6, WL 184C: Removed damaged area from BS 178 bulkhead installed repair on 178 bulhead pressure web LBL .6 WL 184 IAW AWA ER 15-5313-01198-SS5SDR AWXA0002008Web · crackedD: HFEC Indicates .500 crack aftside BS 178 Bulkhead pressure WEB LBL .6, WL 202C: Repaired crack in BS 178 Bulkhead press web IAW AWA ER 15-5313-01198-SS4SDR AWXA0002084Seat Track · nickedD: Nicks on LBL 24.75 seat track at various locations from STA 360-947C: Nicks blended and assessed per SRM 53-10-1 pg 18 STA 520-540 track replaced per SRM 51-30-2 pg 8SDR AWXA0002062Web · crackedD: Cockpit floor web cracked, BS 180, LBL 22, WL 207 at edge of cut-outC: Removed & replaced cockpit floor web IAW AWA ER #15-5311-01186-SS3 at BS 180, WL 207, LBL 22SDR AWXA0002017Web · crackedD: Web cracked at BS 708, RBL 25C: Repaired floor beam web at BS 708, RBL 25 IAW AWA ER 15-5715-01195-SS1SDR AWXA0002061Strap · crackedD: BS 178 Bulkhead web fwd side, BL0 strap cracked, WL 184C: Fabricated Strap IAW boeing DWG # 65-16300 and installed strap IAW B737 SRM 51-30-2 pg 2 at BS 178, WL 184, BL0SDR AWXA0002060Intercostal · crackedLT INTERCOSTAL CRACKED, LBL 24, WL 195, AFT SIDE BELOW FLOOR, BS 178 BULKHEAD. REMOVED AND REPLACED LT INTERCOSTAL IAW B737 SRM 51-30-2 PG 2 AT LBL 24, WL 195, BS 178.SDR AWXA0002059Intercostal · crackedBS 178 BULKHEAD, RT INTERCOSTAL CRACKED, WL 195, RBL 23. REMOVED AND REPLACED RT INTERCOSTAL AT BS 178, WL 195, RBL 23 IAW B737 SRM 51-30-2 PG 2-3.SDR AWXA0002058Web · crackedD: Cockpit floor web cracked, BS 180, RBL 22, WL 207 at edge of cut-outC: removed & replaced floor web at BS 180, RBL 22, WL 207 IAW AWA ER 15-5311-01186-SS3SDR AWXA0002016Web · crackedD: HFEC Indicates 1.3" crack, BS 178 Bulkhead web, FWD side along strap, WL 226.3 RBL 6.8C: Repaired BS 178 bulkhead web at WL 226.3 RBL 6.8 & 4.9 IAW B737 SRM 53-1011 Pgs 1-7SDR AWXA0002015Web · crackedD: BS 178 Bulkhead web side cracked .200" out of button-head rivet hole, WL .234 RBL 10C: Repaired BS 178 Bulkhead web fwd side WL 234 RBL 10 IAW B737 SRM 53-10-11 Pgs 1-6 Fig 1SDR AWXA0002125Frame · crackedLEFT BS 178 CHORD CRACKED AT WL 195 LBL 24. REMOVED AND REPLACED LEFT BS 178 CHORD IAW AWA ER 15-5311-01185-SS1 AND AWA ER 15-5313-01200-JS1.SDR AWXA0002014Web · crackedD: HFEC Indicators(2EA) cracks at hi-lock fastners LBL 8 & 9, WL 234 BS 178 Bulkhead Web FWD sideC: Repaired BS 178 Bulkhead WEB IAW B737 SRM 53-10-11 Pgs 1-7at WL 234, LBL 8,9SDR AWXA0002121Strap · crackedD: Strap cracked on fwd side of BS 178 bulkhead BL-0 WL 188C: Removed and replaced strap IAW DWG 65-16300 and B737 SRM 51-30-2SDR AWXA0002156Splice · corrodedDURING INSPECTION FOUND STRINGER SPLICE AT BS 360 STR 27R CORRODED. REMOVED AND REPLACED STRINGER SPLICE BS 360 AT STR 27R IAW B737 SRM 51-30-2.SDR AWXA0002124Frame · crackedRIGHT BS 178 CHORD CRACKED AT WL 207 RBL 24. REMOVED AND REPLACED CHORD IAW ER 15-5311-01185-SS1.SDR AWXA0002122Doubler · crackedD: Doubler on floor beam at BS 670 LBL 24 crackedC: Removed and replaced doubler IAW B737 SRM 51-30-5 Pg 5SDR AWXA0002057Web · crackedD: Floor beam web cracked 5 places BS 706-716 BL-0.C: Repaired floor beam web IAW AWA ER 15-5715-01193-SS2SDR AWXA0002013Strap · crackedD: Strap cracked on FWD side of BS 178 Bulkhead BL-0 WL 188C: Removed and replaced strap IAW BAC DWG 65-16300 and B737 SRM 51-30-2SDR AWXA0002012Frame · crackedRIGHT BS 178 CHORD CRACKED AT WL 207 RBL 24. REMOVED AND REPLACED CHORD IAW ER 15-5311-01185-SS1.SDR AWXA0002009Beam · crackedD: Aft lower cargo door lower beam Tee cracked 1" at aft end BS 838C: Repaired aft lower cargo door Tower beam Tee at aft BS 838 IAW E.O. 52-33-01SDR AWXA0002006Doubler · crackedD: Doubler on floor beam at BS 670 LBL 24 cracked.C: Removed and replaced doubler IAW B737 SRM 51-30-05 pg 5SDR AWXA0002081Web · crackedD: Bulkhead 178 intercostal on LH side cracked @ WL 207 aft side chord NDT confirmed.C: Web replaced per ref DWG 65-45833-40 & SRM 51-30-2 Pg 5 alodine & primed per SRM 51-10-2 Pg 7SDR AWXA0002045Frame · crackedBS 178 PRESSURE BULKHEAD LEFT HAND CHORD CRACKED AT WL 195 AFT SIDE IN RADIUS. REMOVED AND REPLACED LEFT HAND CHORD AT BS 178 (P/N 65-16300-301) IAW ER 15-5311-01186-SS2.SDR AWXA0002129Angle · corrodedD: During "D" check inspection found frame angle aft side 1088 bulkhead, top side of torque box at duct inlet corrodedC: Removed and replaced frame angle aft side 1088 Bulkhead top side or torque box at duct inlet IAW B737 SRM 51-30-2SDR AWXA0002063Floorbeam · crackedBS 725 BL 24LT SEAT TRACK LOWER ATTACH FLANGE CRACKED. REMOVED CRACK FROM SEAT TRACK LOWER ATTACH FLANGE, INSTALLED REPAIR ON SEAT TRACK LOWER ATTACH FLANGE IAW ER 15-5715-01202-DL3.SDR AWXA0002079Stringer · corrodedD: Aft pit exfoliation corrosion STA 727A STR 26LC: replaced damaged section of STR from 727 to midway between STA 727A & 727B & splice per SRM 53-10-3 Fig 1 DET. 6 or DET 7SDR AWXA0002142Frame · crackedD: Frame cracked at lower fastener hole BS 616 between LT STR 17 & 18SDR AWXA0002083Stiffener · crackedBULKHEAD 178 VERTICAL CHORD AT LBL 5.7 CRACKED IN RADIUS AT WL 190 NDT CONFIRMED. REPAIRED PER REF SRM 53-10-11 FIG 8 SMT 1-20 HFEC PER 737 NDT PT.6 51-00-00. PARTS CAD PLATED ON WIP R445976 REPROTECT PARTS PER SRM 51-10-2. SEALED PER SRM 51-20-4 PG 4, INSTSDR AWXA0002080Frame · crackedBULKHEAD 178 CHORD CRACKED AT WL 207 LT SIDE ABOVE AND BELOW FLOOR -NDT- CONFIRMED. LEFT LWR CHORD P/N 65-16300-86 REPLACED PER REF DWG 65-16300 & SRM 51-30-2 PG 2-3. RESTORED SURFACE FINISH PER AWA 51-21-0 PG 1 & SRM 51-20-4 PG 4.SDR AWXA0002055Angle · crackedD: Cabin center wing box area lower attach angle cracked STA 674 RBL 45C: Repaired cabin center wing box area lower attach angle B.L 45R BS 674 IAW ER 155715-01200 OL3SDR AWXA0002039Beam · crackedD: cabin center wing box area upper attach angle cracked at access cut out STA 665 LBL 24C: repaired cabin center wing box area upper attach angle at access cut out STA 665 LBL 24 IAW ER 15-571507202-OL3SDR AWXA0002018Angle · crackedD: Cabin center wing box area angle cracked STA 663 RBL 24C: Cut out cracked area fabricated repair cord segment, splice angles & straps heated primed and installed repair cord segment, splice angles & straps IAW B737 200 SRM 51-30-2 pg 7 & 8 and AWA ER 15-571SDR AWXA0002010Angle · crackedD: Cabin center wing box area attach angle cracked STA 674 RBL 45C: Repaired cabin center wing box area lower attach angle BL 45R BS 674 IAW ER 15-5715-01200 DL3SDR AWXA0002150Frame · crackedLOWER T-CHORD CRACKED BS 717 BL 0 BELOW CABIN FLOOR. REPAIRED IAW AWA ER 15-5702-01209-DD2.SDR AWXA0002126Angle · corrodedD: R/H torque box aft side duct support angle corroded at screw holes approx BS 1130 on side web of torque boxC: Removed and replaced support angle at R/H torque box B.S. 1130 IAW 737 SRM 51-30-2 Pgs 2,3 & 32SDR AWXA0002091Bulkhead · crackedINSP OF STA 178 BLKHD FWD FACE REVEALS SEVEN CRACK INDICATIONS. LOCATIONS ARE AS FOLLOWS LBL 8/WL 228, LBL 4/WL 216, RBL 12/WL 216, LBL 12/ WL 216, LBL 1/WL 200, RBL 1/WL187, & LBL 1/WL 187. REPAIRED PER ER NR 15-5313-01212-DD1 HFEC PER 737 NDT MAN, PT 6 51-SDR AWXA0002075Floorbeam · crackedLOWER T-CHORD CRACKED BS 717 BL 0 BELOW CABIN FLOOR. REPAIRED IAW AWA ER 15-5702-01209-DD2.SDR AWXA0002019Door Frame · crackedFWD CARGO DOOR LOWER CORNER FRAME CRACKED AT AFT LOWER STOP FITTING. REMOVED AND REPLACED LOWER AFT CORNER FRAME AT FWD CARGO DOOR IAW EO 52-31-04.
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