Boeing MD-90-30

Service difficulty reports · 6,066

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 = 'MD9030'
  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.

SDR DALA2020080602719Attach Angle · crackedCRACK ON RH ATTACH ANGLE THROUGH ACCESS PANEL 370AL. NRC 00156: RH ATTACH ANGLE WAS REPLACED IAW DWG #5912188 REV BD AND MD-90 SRM 51-30-02 AND 51-30-05 VOL.II.Aug 5, 2020 · N963DN · Doug MD9030 · Empennage StructureSDR DALA2020080542718Frame · crackedCRACK ON FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT (CAT). NRC 00251: FRAME STA 1458 AND LONG 1 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER MD-90 SRM 53-10-02 FIG 1 VOL I. (LP #1589387)Aug 4, 2020 · N963DN · Doug MD9030 · Fuselage Main, FrameSDR DALA2020030601662Battery Pack · dischargedFOUND LWR EMERGENCY PATH LIGHTS ON BOTH FWD DOORS INOP. R/R EMERGENCY LIGHT SLID AND BATTERY PACK B5-211 PER MD90 AM;33 -51. OPS CHECK GOOD . A/C OK FOR SVC. (6954427)Mar 5, 2020 · N919DN · Doug MD9030 · Emergency LightingSDR DALA2020030301548Fastener · missingLOOSE AND MISSING FASTENERS ABOVE SPLICE STA ZFS= 52.267 AT VERTICAL STABILIZER LEADING EDGE (EHV) SUMMARY NRC 00491: VERTICAL STABILIZER LEADING EDGE WAS REPAIRED PER MD-90 SRM 55-30-05 VOLUME I PAR. 11, AD 5530-01044-05 AND DWG SG09550004 REV. D. PERFORM DVIFeb 25, 2020 · N908DA · Doug MD9030 · Vertical Stabilizer, Plate/SkinSDR DALA2020022601419Beam · crackedINITIAL INSPECTION: CRACKED RH DOOR JAMB BEAM ON STA 45 AND X=- 18 AT NLG WHEEL WELL AREA (FYT) ENTR 00983062 W SUMMARY OF NRC 600:RH DOOR JAMB BEAM ON STA 45 AND X=-18 AT NLG WHEEL WELL AREA WAS REPAIRED PER ETI-90-20-020 REV 2 AND ER/A 585590-14 REV. ORIGINAFeb 25, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020022501377Fan · failedLEFT HEAT EXCHANGER COOLING FAN POPS ALL 3 PHSES C/B'S. ODOR THROUGHOUT CABIN C/A R/R LT HEAT EXCHANGER COOLING FAN PER MD90AMM 21-55. LEAK AND FUNCTIONAL CKS GOOD (5498218)Feb 24, 2020 · N931DN · Doug MD9030 · Air Distribution FanSDR DALA2020022431349Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA Y=1437 BTW LONG 13-13RH (FUS) SUMMARY OF NRC S/N 00161: FUSELAGE SKIN STA Y=1437 BTW LONG 13- 13RH WAS REPAIRED PER ER/A 585546-14 REV. ORIGINAL AND ETI-90-20 -016 REV. 1 AND PERFORM DETAIL VISUAL INSPECTION WITHIFeb 22, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020022421348Skin · damagedINITIAL INSPECTION: WORN AND BENTED PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN ON L1 DOOR HOLD OPEN ATTACH POINT (FUS) SUMMARY OF NRC 00100. PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN ON L1 DOOR HOLD OPEN ATTACH POINT WAS REPLACED PER MD 90 SRM 51- 30-05 VOL. II AFeb 21, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020022421347Torque Tube · crackedCRACKED VENTRAL STAIR WAY TORQUE TUBE BEAM AT AFT ACCESSORY COMPARTMENT (CAT) LOG-PAGE UPDATED SUMMARY OF NRC 00794. VENTRAL STAIR WAY TORQUE TUBE BEAM AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER MD 90 SRM 51-30-02, 51-30 -05 AND 51-30-01 VOL. II ALSO D/DWG Feb 21, 2020 · N908DA · Doug MD9030 · Entrance StairsSDR DALA2020022421346Floor Support · corrodedCORROSION ON L2 LOWER SILL INTERCOSTAL BTW STA 720/740 AND 63 LBL PASSENGER CABIN (W2) LOG-PAGE UPDATED SUMMARY OF NRC 00359 CORROSION LEVEL 2 LOWER SILL BTW STA 720/ 740, 63 LBL WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 AND 7 (1499637)Feb 21, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020022101310Door Frame · corrodedCORROSION ON DOOR JAMB WEB STA 1212-1220 BTW PROJECTION LONGS 29RH-28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 SUMMARY OF NRC 00334: CORROSION LEVEL 2: WEB OF STA. 1204 TO 1276 BTW. LONG. 26 R/H TO LONG. 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 VOL. Feb 20, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020022101309Skin · corrodedCORROSION ON FUSELAJE SKIN STA=864 AND STR- 28R TO STR- 29R. SUMMARY OF NRC 00198: CORROSION (LEVEL 2) ON FUSELAJE SKIN STA= 864 AND STR- 28R TO STR- 29R WAS REPAIRED PER ETI-90-20-009 REV. ORIGINAL AND ER/A 585513-14 REV. ORIGINAL SECTION I. ACCORDING TO ER/AFeb 20, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021901242Coffeemaker · failedDURING CLIMB, FLT ATTEND'S SMELLED ODOR FROM COFFEE MKR. COFFEE MAKER WAS EXTREMELY HOT, SMELLED LIKE ELECTRICAL BURN NEAR CKPT DOOR. I TURNED OFF GALLEY PWR. ALSO WALL AT COAT/HAT RACK WAS HOT TO THE TOUCH. AFTER GALLEY PWR WAS TURNED OFF FOR, ODOR WENT AWAY.Feb 19, 2020 · N926DH · Doug MD9030 · Buffet/GalleysSDR DALA2020021901238Door Frame · crackedINITIAL INSPECTION: CRACKED LH DOOR JAMB BEAM ON STA 48 AND X=18 AT NLG WHEEL WELL AREA (FYT) LOG-PAGE UPDATED SUMMARY OF NRC 00601: LH DOOR JAMB BEAM ON STA 48 AND X=18 AT NLG WHEEL WELL AREA WAS REPAIRED PER MD-90 VOL. I SRM 53-90-01 PAR.8 LOG-PAGE UPDATED (Feb 19, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021901246Longeron · crackedINITIAL INSPECTION: CRACKED LONGERON 2RH ON STA 1475 AT AFT ACCESSORY COMPARTMENT (CAT) SUMMARY OF NRC S/N 00785: LONGERON WAS REPAIRED PER ER/A 564080- 14MA REV. ORIG. SECTION II. PERFORM SECTION III INSPECTION EVERY 3000 CYCLES AFTER THIS REPAIR. PER ER/A 56Feb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Longeron/StringerSDR DALA2020021901241Skin · corrodedAWR HIDDEN CORROSION IN REF NRC 895. DURING REMOTION OF VAPOR BARRIER WAS FOUND CORROSION ON CENTER WING UPPER SKIN STA 943- 962 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 01179: CORROSION LEVEL 1; CORROSION ON CENTER WING UPPER SFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021901240Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 992 BTW X=44 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF NRC 00891. CORROSION LEVEL 1. CORROSION ON CENTER WING UPPER SKIN STA 992 BTW X=44 AT WING BOX AREA WAS REMOVED PER MD-90 SRM 51-10-03 PARFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021901239Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY. OF NRC 0888. CORROSION LEVEL I. CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=44 TO X=60 AT WING BOX AREA WAS REMOFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021801200Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00884, CORROSION LEVEL 1 , CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=-44 TO X=-60 AT WING BOX AREA WAFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021801199Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00885, CORROSION LEVEL 1; CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=-44 TO X=-60 AT WING BOX AREA WASFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021801198Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ; OF NRC 889, CORROSION LEVEL 1 ; CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=44 TO X=60 AT WING BOX AREA WAS ATTFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021801197Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 943 TO 962 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ;OF NRC 00890, CORROSION LEVEL 1 : CORROSION ON CENTER WING UPPER SKIN STA 943 TO 962 BTW X=44 TO X=60 AT WING BOX AREA WAS ATFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021801196Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 883 TO 902 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00887: CORROSION WAS ATTENDED PER MD-90 SRM 51-10-03 PAR 26 (A) VOL. II ETI-90-20-008 REV. 1 AND ER/A 585247 -14 REFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021801195Skin · corrodedINITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 962 TO 984 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00886: CORROSION WAS ATTENDED PER MD-90 SRM 51-10-03 PAR 26 VOL. II AND ETI-90-20-007 REV. ORIG AND ER/A 585124-1Feb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021801194Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL STA 1205-1210 BTW LONGS 30 AND 29RH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00349: CORROSION LEVEL 1: CORROSION ON INTERCOSTAL STA 1205 TO 1210 BTW LONGS 30 TO 29 RH AT AFT CARGO COMPARTMENT WAS Feb 18, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020021801193Frame Angle · corrodedINITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1379 BTW LONGS 29RH TO 26RH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00552: FRAME CLIP STA 1379 BTW LONGS 29RH TO 26RH AT AFT CARGO COMPARTMENT (CCT) WAS REPLACED PER MD-90 SRM VOL I 53-10-02 FFeb 18, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021761187Frame Angle · corrodedINITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1364 BTW LONGS 28RH TO 27LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00303. CORROSION LEVEL 2. FRAME CLIP STA 1364 BTW LONGS 28RH TO 27LH WAS REPLACED PER MD90 SRM 51-30-02 VOL.II AND D/DWG 991Feb 16, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021761186Frame Angle · corrodedINITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1269 BTW LONGS 29RH TO 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00328: CORROSION LEVEL 2. FRAME CLIP STA 1269 BTW LONG. 29 RH TO 28 WAS REPLACED PER MD 90 SRM VOL.I 53-10-02 PAR . 5 FIG. 3Feb 16, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021761185Longeron · corrodedINITIAL INSPECTION: CORROSION ON LONGERON END 27RH STA 1395 AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) LOG-PAGE UPDATED RII: N ENTR 00897853 W SUMMARY OF NRC 00558. CORROSION LEVEL 2. LONGERON END 27RH STA 1395 AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90Feb 16, 2020 · N908DA · Doug MD9030 · Fuselage Main, Longeron/StringerSDR DALA2020021761184Longeron · corrodedINITIAL INSPECTION: CORROSION ON LONGERON END 28RH STA 1395 AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00557. CORROSION LEVEL 2 LONGERON END 28RH BTW STA 1395 AT AFT CARGO COMPARTMENT WAS REPLACED PER MD90 VOL. LL SRM 51-30-05 AND D/DWG 593643Feb 16, 2020 · N908DA · Doug MD9030 · Fuselage Main, Longeron/StringerSDR DALA2020021761183Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA Y=1494 BTW LONG 2 -3 LH (FUS) LOG-PAGE UPDATED SUMMARY OF NRC 00591: SKIN STA Y=1494 BTW LONG 2-3 LH WAS REPAIRED PER ER/A 585379-14 REV. ORIG AND ETI-90-20-002 REV. 1 PERFORM A GENERAL VISUAL INSPECTION PER ER/A Feb 15, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021761182Skin · corrodedINITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00555. CORROSION LEVEL 2 PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT WAS REFeb 15, 2020 · N908DA · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2020021761181Structure · corrodedINITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00555. CORROSION LEVEL 2 PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT WAS REFeb 15, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021761180Door Frame · corrodedINITIAL INSPECTION: CORROSION ON DOOR JAMB WEB STA 360-370 BTW LONGS 28RH AND 26RH AT FWD CARGO COMPARTMENT MRB 53-302-07 (CCD) SUMMARY ; OF NRC 00827 ; LEVEL CORROSION 2 . DOOR JAMB WEB STA 360-370 BTW LONGS 28RH AND 26RH AT FWD CARGO COMPARTMENT WAS REPAIREDFeb 15, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021761179Seat Track · corrodedINITIAL INSPECTION: CORROSION ON LH SEAT TRACK X=54 STA 745-750, 765-770, 775-780, 795,800, 805-810 AND 825-840 MRB 53-211-02 ( CPAX) SUMMARY ; OF NRC 103 ; NEW SECTION SEAT TRACK ON STA Y=598 TO 864 WAS REPLACED PER MD-90 SRM 53-40-01 PAR .10 FIG . 6 VOL. I LFeb 15, 2020 · N908DA · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020021761178Seat Track · corrodedINITIAL INSPECTION: CORROSION ON LH SEAT TRACK X=54 STA 620-625, 640-650, 670-675, 690-695, 700-705, 710-715 AND 730-735 MRB 53- 211-02 (CPAX) SUMMARY ; OF NRC 102 ; NEW SECTION SEAT TRACK ON STA Y=598 TO 864 WAS REPLACED PER MD-90 SRM 53-40-01 PAR .10 FIG . 6Feb 15, 2020 · N908DA · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020021401139Pan · crackedINITIAL INSPECTION: CRACK ON LH AFT EMERGENCY EXIT DOOR JAMB PAN UPPER AREA (FUS) SUMMARY OF NRC 00162. LH AFT EMERGENCY EXIT DOOR JAMB PAN UPPER AREA (FUS) WAS REPAIRED PER MD 90 SRM 53-60-02 FIG. 4. LOG-PAGE UPDATED (1488821)Feb 14, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021401140Door Frame · corrodedCORROSION ON MID CARGO COMPT LOWER DOOR JAMB STA 695 TO 750 MRB 53-122-02 (CCC) SUMMARY OF NR 00206. LEVEL CORROSION II. MID CARGO COMPT LOWER DOOR JAMB STA 695 TO 750 WAS REPAIRED PER MD90 SRM VOL I 53-60- 02 FIG 9. SRM VOL II 51-10-03 PAR 21, 14 AND 26. (MRBFeb 13, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021401138Frame · crackedCRACK ON CAP STA Y= 1364 LONG 7LH AT PASSENGER CABIN (CPAX) SUMMARY OF NRC S/N 01063: CAP STA Y= 1364 LONG 7LH AT PASSENGER CABIN WAS REPAIRED PER ER/A 585192-14 REV. ORIGINAL AND ETI-90- 20-004 REV, ORIGINAL ASSOCIATED ER/A 00-585192 ADDED FOR AC 9208 (148870Feb 13, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021401137Frame · corrodedCORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT). SUMMARY OF NRC 00554. CORROSION LEVEL 2 PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRFeb 13, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021301108Hydraulic System · leakingUPON LANDING RIGHT HYDRAULIC QUANTITY RAPIDLY DROPPED TO 4 QTS. F/A NOTIFIED US DURING TAXI A SMELL OF HYDRAULIC FLUID BURNING C/A VERIFIED LEAK FROM TAIL DRAINS FWD OF APU INLET. INLET CONTAMINATED (246850) FOUND ELEV ACCUM. BYPASSING AND HYD ELEV PRESS GAUGEFeb 12, 2020 · N913DN · Doug MD9030 · Hydraulic System, MainSDR DALA2020021301107Channel · corrodedCORROSION ON PREVIOUS REPAIR CHANNEL AND STRAP FRAME STA 1344 BTW LONGS 28RH TO 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) NRC 00301. CORROSION LEVEL 2 PREVIOUS REPAIR CHANNEL AND STRAP FRAME STA 1344 BTW LONGS 28RH TO 28LH AT AFT CARGO COMPARTMENT WAS Feb 12, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021101075Fitting · corrodedCORROSION ON FWD AND AFT FITTING AT AFT CARGO COMPT LOWER DOOR JAMB STA 1211 AND 1268 (CCT) MRB 53-123- 02 NRC 00202. CORROSION LEVEL 2. FITTING AT AFT CARGO COMPARTMENT LOWER DOOR JAMB STA Y=1211 AND Y=1268 WERE REPLACED PER MD 90 SRM 51-30-05 VOL. I AND D/DWFeb 11, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021101074Cusp Web · corrodedCORROSION ON RH CUSP WEB BTW STA 718-736 BTW X=-44 AND X=-60 MRB 53?211?01 (CPAX) SUMMARY OF NRC 01239: (LEVEL CORROSION 2), SECTION RH CUSP WEB OUT LIMIT BTW STA 718-736 BTW X=-44 AND X=-60 WAS REPAIRED PER MD-90 VOL II SRM 53-20-02 FIG 27 LOG-PAGE UPDATED (1Feb 10, 2020 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2020021101073Frame · corrodedCORROSION ON PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) NRC 00550. CORROSION LEVEL 2. PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM VOL I 53-Feb 10, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021101072Skin · damagedRE-WRITE FROM NRC 0415: INITIAL INSPECTION: BEND EXTERNAL LOWER PREVIOUS REPAIR AT FWD ENTRANCE DOOR (L1) (PTAS)". REASON FOR RE-WRITE: PREVIOUS REPAIR CANT BE CONFORMED.SUMMARY OF NRC 1132: EXTERNAL LOWER SKIN AT FWD ENTRANCE DOOR ( L1) WAS REPAIRED PER MD-90Feb 10, 2020 · N908DA · Doug MD9030 · Passenger/Crew DoorsSDR DALA2020021101071Frame · corrodedCORROSION ON PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00549. CORROSION LEVEL 2.PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRMFeb 10, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021101070Frame Angle · corrodedCORROSION ON FRAME CLIP AT AFT CARGO COMPARTMENT STA 1344 AND BETWEEN L27-R AND L26-R. (C3) CORROSION LEVEL 2: FRAME CLIP AT AFT CARGO COMPARTMENT STA 1344 AND BETWEEN L27-R AND L26-R WAS REPAIRED PER MD-90 SRM VOL I 53-10-02 FIG.3. (UT) WAS ACCOMPLISHED PER NFeb 10, 2020 · N908DA · Doug MD9030 · Fuselage Main, FrameSDR DALA2020021101069Window Frame · crackedCRACK ON FRAME OF CLEAR VIEW WINDOW LH, UPPER AFT CORNER. (CPIL) INTERNAL DOUBLER WAS REPLACED PER MD90 SRM VOL II 51-30-02 AND 51-30-05 AND DWG 5911356 REV. DJ. (1483970)Feb 10, 2020 · N908DA · Doug MD9030 · Fuselage Main, StructureSDR DALA2020021001037Window Frame · crackedAWR HIDDEN CRACK: IN REF NRC 01010 AFTER DOUBLER WAS REMOVED HIDDEN CRACK WAS FOUND ON UPPER AFT SKIN CORNER OF RH CLEARVIEW WINDOW (CPIL) SUMMARY NRC 01243:UPPER AFT SKIN CORNER OF RH CLEARVIEW WINDOW WAS REPAIRED PER MD 90 SRM VOL.I 56-10-02 FIG. 1 (ET) (HFEFeb 9, 2020 · N908DA · Doug MD9030 · Fuselage Main, Structure
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