Boeing 727-22
Service difficulty reports · 1,282
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 = '72722' 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 = '72722' 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 96FDEA00694Skin · corrodedWHILE WORKING NR0602, FOUND SKIN AND BONDED DOUBLER TO HAVE CORROSION ON MATING SURFACES AT BS 1110 TO 1128 FROM STR 25 TO 26R. REMOVED CORROSION FROM BLER AND TRIPLER. DAMAGE ON TRIPLER WAS OUT OF LIMITS. FABRICATED NEW TRIPLER, ALODINED AND PRIMED TRIPLERSDR 96FDEA00689Frame · double drilledDOUBLE DRILLED HOLES ON NESTLED FLANGE OF FRAME AT BS 1166 LBL 20 WL 159. TRIMMED DAMAGE AND INSTALLED DOUBLER PER FEDEX SRM 51-40-3.SDR 96FDEA00688Keel Beam · corrodedCORROSION (C53-113-01, 2) ON LT KEEL BEAM AT LBL 6 WL 190 BS 979, 1013 AND 1030. ALSO, MATERIAL CHIPPED AWAY FROM BEAM AT 1031. FABRICATED REPAIR PARTS AND INSTALLED PER EA 7-5310-28043.SDR 96FDEA00687Stringer · corrodedUPON REMOVAL OF SPLICE AT BS 520, DISCOVERED CORROSION OF STR 27R BS 522 AND 517 TO BE OUT LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF STR 27R.SDR 96FDEA00686Skin · corrodedCORROSION (C53-132-02, 1) ON INNER SURFACE OF WING CENTER SECTION UPPER SKIN BS 870 RBL TO LBL 70 PLUS ON RT SURFACE LBL 55 TO 70. REMOVED CORROSION AND BLENDED AREA, WITHIN LIMITS PER EA 7-5710-28042.SDR 96FDEA00685Web · crackedUPON REMOVAL OF I/B FLOOR WEB AT BS 294 TO 344 WL 169 RBL 15 TO 27 FOUND TO BE CRACKED. REMOVED AND REPLACED FLOOR WEB AND INSTALLED ALL BRACKETS AND ANGLES REMOVED FOR INSTALLATION AT BS 294 TO 351 WL 169 RBL 15 TO 27. ALL WORK IAW BAC DRW NR 65-18915.SDR 96FDEA00684Web · crackedWHILE WORKING NR0498, FOUND O/B RT DOGHOUSE WEB TO BE CRACKED BS 294 TO 351 RBL 25 AND 26 WL 169. REMOVED AND REPLACED O/B DOGHOUSE WEB ALL WORK IAW BAC DRW NR 65-18915 AT BS 294 TO 351 RBL 25 TO 36 WL 169.SDR 96FDEA00691Skin · gougeBS 277.2 STR 21R WL 180, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE IN SKIN AT BS 277.2 STR 21R WL 180 ORIGINAL SKIN THICKNESS WAS .040, AREA REMOVED WAS .030. A 1 INCH BY .5 INCH AREA AND WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. DAMAGED AREA SDR 96FDEA00690Skin · dentedBS 660.3 STR 20R WL 181, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE AT BS 660.3 STR 20R WL 181 WAS OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED 2.75 INCH BY 1.8 INCH OF DAMAGED SKIN, FABRICATED DOUBLE AND INSTALLED IAW FEDEX SRM 53-30-3.SDR 96FDEA0539Frame · double drilledDOUBLE DRILLED HOLES ON THE NESTLED FLANGE OF FRAME AT BS 1110 LBL 19 WL 152. TRIMMED DAMAGE AND INSTALLED DOUBLER PER FEDEX SRM 51-40-3.SDR 96FDEA00602Tripler · corrodedNR 0074 AND 027, BS 1110 RBL 29 BETWEEN STR 25 TO 26R SKIN BULGE AROUND FASTENERS. REPAIRED DAMAGED SKIN IAW FEDEX EA 7-5310-28049.SDR 96FDEA00601Transverse Beam · crackedNR 0248 AND 028, FWD CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN O/B RADIUS 12 INCHES AND 24 INCHES OF FWD EDGE. REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON FWD CARGO DOOR MM 52-31-61.SDR 96FDEA00600Web · crackedNR 0254 AND 029, AFT CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN RADIUS 24 INCHES AFT OF FWD EDGE OF DOOR. REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON AFT CARGO DOOR.SDR 96FDEA00597Skin · delaminatedNR 0411 AND 035, RT WING O/B AFT FLAP HAS AN AREA OF DELAMINATION ON LOWER SKIN 60 INCHES FROM I/B END. REPAIRED DAMAGED LOWER SURFACE SRM 51-40-6.SDR 96FDEA00595Frame · double drilledNR0473, DOUBLE DRILLED HOLES ON NESTLED FLANGE OF FRAME AT BS 1166 LBL 20 WL 159. *S/D* TRIMMED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3.SDR 96FDEA00594Frame · double drilledNR 0474 AND 038, DOUBLE DRILLED HOLES ON FRAME AT BS 1148 LBL 20 WL 156. REPAIRED DOUBLE DRILLED HOLES PER SRM 51-40-3.SDR 96FDEA00593Angle · crackedNR0500 AND 042, CRACK FOUND IN BS 740 SILL REINFORCEMENT ANGLE FWD WL 170 LBL 38. REPAIRED 740 SILL ANGLE PER SRM 51-20-1 AND 51-40-3.SDR 96FDEA00592Blkhd Web · corrodedNR 0518 AND 043, WHILE WORKING NR 0468 FOUND AFT BULKHEAD OF WING CENTER SECTION TO BE CORRODED BS 870 LBL TO RBL 65 WL 178. REMOVED DAMAGED WEB AND INSTALLED NEW WEB AT BS 870 WL 162 TO 188 RBL 65 TO LBL 65.SDR 96FDEA00590Angle · crackedNR 0540 AND 045, WHILE WORKING NR 0254 FOUND AFT CARGO DOOR NR 2 FROM BOTTOM, I/B L-ANGLE TO BE CRACKED IN RADIUS. REMOVED AND REPLACED L-ANGLE SRM 52-30-1.SDR 96FDEA00589Web · corrodedNR 0558 AND 047, UPON REMOVAL OF LT I/B DOGHOUSE WEB, FOUND IT TO BE OUT OF LIMITS AT BS 294 TO 344 LBL 15 TO 23 WL 159. REMOVED AND REPLACED LT I/B DOGHOUSE WEB AND REINSTALLED ALL DUCTS AND BRACKETS THAT WERE REMOVED FOR INSTALLATION AT BS 294 TO 351 LBL 15SDR 96FDEA00544Frame · crackedCRACK INDICATION NOTED HOLE 2 ROW 2 BS 870 LT. REMOVED ANGLE, STOP DRILLED CRACK, INSTALLED ANGLE PER SB 727-53-194 AND ER 031496LD2.SDR 96FDEA00543Frame · double drilledDOUBLE DRILLED HOLES ON FRAME AT BS 1050 LBL 20 WL 147. TRIMMED DAMAGED AREA AND REPAIRED FRAME PER FEDEX SRM 51-40-3 FIG 1.SDR 96FDEA00542Door Skin · dentedFWD ENTRY DOOR HAS 2 DENTS BY LOWER HINGE CUTOUT AFT SIDE OF DOOR ON EXTERNAL SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 52-00-3.SDR 96FDEA00541Strap · corrodedCORROSION (C53-113-01) ON THRESHOLD VERTICAL WEB, BS 540 AND 560 RBL 21 WL 156. REMOVED AND REPLACED VERTICAL WEB SRM 53-10-1.SDR 96FDEA00540Frame · double drilledDOUBLE DRILLED HOLES ON THE NESTLED FLANGE OF A-FRAME AT 1130 LBL 19 WL 154. TRIMMED AND REPAIRED DOUBLE DRILLED HOLES ON NESTLED FLANGE OF A-FRAME AT 1130 LBL 19 WL 154 PER FEDEX SRM 51-40-3.SDR 96FDEA00538Frame · double drilledDOUBLE DRILLED HOLES ON FRAME AT BS 1070 LBL 20 WL 149. TRIMMED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3.SDR 96FDEA00537Frame · crackedWHILE WORKING NR0177, FOUND CRACK IN FRAME AT BS 500 LBL 8 WL 156. REMOVED AND REPLACED ANGLE PER SRM 51-40-3.SDR 96FDEA00588Skin · gougedREMOVED GOUGE IN SKIN AT BS 660 TO 3 STR 20R WL 181, FABRICATED REPAIR DOUBLER IAW 53-30-3.SDR 96FDEA00587Skin · gougedNR 0072 AND 019, BS 219-3 LBL 15 WL 163 THERE IS A DEEP GOUGE IN SKIN. REPAIRED GOUGE IN SKIN SRM 53-30-3 AND 53-30-1.SDR 96FDEA00586Skin · lightning strikeNR0491 AND 022, TWO LIGHTNING STRIKES AT BS 1188 STR 27R AND BS 1183 STR 27R. REPAIRED DAMAGE PER SRM 53-30-3.SDR 96FDEA00585Floor Support · corrodedNR 0209 AND 020) CORROSION ON FLOOR SUPPORT AT BS 515 RBL 9 WL 156. REPAIRED FLOOR SUPPORT SRM 53-10-5.SDR 96FDEA00584Chord · corrodedNR0399 AND 021, CORROSION (C53-113-03) ON LT MID NOSE CHORD VERTICAL FLANGE EMANATING FROM BENEATH VERTICAL STIFFENER AT BS 318, 336 AND 344. TWO BULGES IN FLOOR WEB ON CHORD HORIZONTAL FLANGE AT BS 318 AND 336 LBL 15 WL 169, ACCESS REQUIRED.SDR 96FDEA00583Web · corrodedNR0496 AND 023, CORROSION (C53-224-03-1/2) NOSE E-BAY WEB IS CORRODED STA 212 TO 221 RBL 26 WL 178.SDR 96FDEA00582Doubler · corrodedNR 0527 AND 025, CORROSION (C53-132-02, 1) ON ACCESS HOLE DOUBLER BS 875 WL 184 RBL 63. FABRICATED AND REPLACED DOUBLER ON ACCESS DOOR, SRM 53-10-1.SDR 96FDEA00581Filler · corrodedNR 0543 AND 026, WHILE WORKING NR 0221, DISCOVERED CORROSION ON SKIN FROM BS 1059 TO 1097 BETWEEN STR 25 AND 26R RBL 32 TO 39 WL 149. REMOVED CORROSION, FABRICATED FILLER AND INSTALLED, SRM 53-30-1.SDR 96FDEA00536Angle · crackedWHILE WORKING NR0254, FOUND AFT CARGO DOOR NR 3 FROM BOTTOM, O/B L-ANGLE TO BE CRACKED IN RADIUS. REMOVED AND REPLACED AFT CARGO DOOR NR 3 O/B L-ANGLE.SDR 96FDEA00533Doubler · corrodedCORROSION (C53-132-02, 1) ON ACCESS HOLE DOUBLER BS 875 WL 184 LBL 63. FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-01. FABRICATED AND REPLACED ACCESS HOLE DOUBLER AT BS 875 WL 184 LBL 63.SDR 96FDEA00518Radome · chippedWHILE WORKING CARD 71C102-01, FOUND RADOME TO BE MISALIGNED AT BS 178 ALLOWING RADOME TO CATCH DOUBLER WHICH CRACKED DOUBLER AND CHIPPED RADOME WL 285, LBL 4. REPAIRED RADOME WL 285 LBL 4, PER SRM 53-50-4 AND REPAIRED SKIN DOUBLER AT BS 178 WL 235 LBL 4 PER ESDR 96FDEA00519Skin · crackedWHILE PERFORMING PRESSURIZATION DISCOVERED CRACK IN EXTERIOR SKIN BS 423, JUST BELOW STR 23 RT. REPAIRED EXTERIOR SKIN IAW SRM 53-30-3 FIG 2.SDR 96FDEA00555Spar Chord · corrosionCORROSION (C53-132-02) ON THE WING CENTER SECTION REAR LOWER CHORD, STA 870 LBL 20 TO 26 WL 140. REMOVED AND REPLACED LOWER CHORD PER FEDEX EA 7-5710-27481.SDR 96FDEA00554Spar Chord · corrosionCORROSION (C53-132-02) ON THE WING CENTER SECTION REAR UPPER SPAR CHORD, STA 870 LBL 30 RBL 30 WL 174. REMOVED AND REPLACED UPPER CHORD PER FEDEX EA 7-5710-27481.SDR 96FDEA00553Intercostal · dentedDENTED INTERCOSTAL BS 1055 BETWEEN STR 23L TO 25L LBL 36 TO 48 WL 156. REMOVED AND REPLACED OUT OF LIMITS INTERCOSTAL PER FEDEX SRM 53-10-1.SDR 96FDEA00552Fitting · corrodedCORROSION ON STR 20L FITTING BS 360 TO 367. REMOVED AND REPLACED CORRODED FITTING PER SB 727-53-0209.SDR 96FDEA00550Fitting · corrodedCORROSION (C53-137-01) BS 1342 RBL 17 STR 5R ON FITTING ANGLE. REMOVED CORRODED TERMINAL FITTING AND INSTALLED NEW RT SPAR TERMINAL FITTING ON VERTICAL STABILIZER AT BS 1342 IAW BOEING SB 727-55-088.SDR 96FDEA00549Shear Web · corrodedCORROSION EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 6 TO LBL 20 WL 208. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1.SDR 96FDEA00548Bullnose · corrosionCORROSION (097-562-01-2) NR 4 K-FLAP BULLNOSE O/B BONDING JUMPER, UPPER ATTACH POINT. REMOVED CORROSION PER FEDEX SRM 57-50-03 AND 27-57-010.SDR 96FDEA00547Shear Tie · damagedMECH DAMAGE ON SHEAR TIE AT BS 600 BETWEEN STR 16 AND 17R. REMOVED AND REPLACED SHEAR TIE SRM 53-10-1.SDR 96FDEA00546Door Frame · gougedFWD ENTRY DOOR LATCH ROLLER RUBS ON DOOR STRUCTURE. REMOVED AND REPLACED FWD SIDE FRAME SRM 53-10-1.SDR 96FDEA00545Skin · creasedBS 366 STR 20R THERE IS A CREASE IN SKIN. REPAIRED CREASE PER FEDEX SRM 53-03-3.SDR 96FDEA00535Spar Chord · corrosionCORROSION (C53-132-02, 1) ON THE WING CENTER SECTION UPPER SPAR CHORD STA 870 LBL TO RBL 60 WL 178. REMOVED AND REPLACED UPPER SPAR CHORD.
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