Boeing 727-223

Service difficulty reports · 5,313

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 = '727223'
  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 C8GA2011000015Carriage · brokenDURING CLIMB OPERATION, THE OTBD FLAPS FROZE AT 3 DEGREES ON CLIMBOUT, 9 UNITS OF AILERON TRIM WAS REQUIRED FOR LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT BOTH RT OTBD FORE FLAP SEJul 29, 2011 · N715AA · Boeing 727223 · Trailing Edge FlapsSDR FOTR2111712633Stringer · corrodedCORROSION ON OTBD SIDE OF STRINGER 28L AT BS 450. REPAIRED ON FASI WO 21117, NR 12633.Jul 29, 2011 · N899AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR CA110802001Line · rupturedDURING APPROACH ON SHORT FINAL THE ACFT HAD LOST ALL HYD FLUID IN SYS A. THE ACFT CONTINUED THE APPROACH AND LANDED WITHOUT FURTHER PROBLEMS. UPON POST-FLIGHT INSP BY MX PERSONNEL, IT WAS DETERMINED THAT 1 LT MLG DOOR ACTUATOR FLEXIBLE LINE RUPTURED AND CAUSJul 28, 2011 · Boeing 727223 · Hydraulic System, MainSDR FOTR2111712782Tab · delaminatedLT ELEVATOR CONTROL TAB HAS A SMALL AREA OF DELAMINATION, REPAIRED ON FASI WO 21117, NR 12782.Jul 27, 2011 · N899AA · Boeing 727223 · Elevator, Tab StructureSDR FOTR2111712656Frame · dentedAFT CARGO COMPARTMENT HAS DENTS AT STA 1010 BETWEEN STR 25R AND 24R. REPAIRED ON FASI WO 21117, NR 12656.Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2111712657Frame · dentedAFT CARGO COMPARTMENT- DENT ON FRAME STA 1030 BETWEEN STR 25R AND 24R. REPAIRED ON FASI WO 21117, NR 12657.Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2111712350Mount Bracket · crackedNR 6 SLAT ACTUATOR ATTACHED MOUNT BRACKET, ON SLAT INBD SIDE IS CRACKED, WS519.0. REPAIRED ON FASI WO 21117, NR 12350.Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge DevicesSDR FOTR2111712661Frame · dentedAFT. CARGO COMPARTMENT- DENT ON FRAME AT STA 1010 AT STR 25L. REPAIRED ON FASI WO 21117, NR 12661.Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2111712345Bracket · crackedNR 7 SLAT ACTUATOR MOUNT INBD BRACKET ON SLAT IS CRACKED. REPAIRED ON FASI WO 21117, NR 12345.Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge DevicesSDR FOTR2111712726Bracket · crackedNR 7 SLAT ACTUATOR MOUNT OTBD BRACKET ON SLAT IS CRACKED, WS629.0. REPAIRED ON FASI WO 21117, NR 12726.Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge DevicesSDR FOTR2111712154Rib · crackedNR 4 SLAT INBD ACTUATOR ROD END ATTACH RIB IS CRACKED, WS383. REPAIRED ON FASI WO 21117, NR12154.Jul 25, 2011 · N899AA · Boeing 727223 · Leading Edge DevicesSDR FOTR2111712669Skin · bentAFT AIRSTAIRS RT EXTERIOR SKIN SURFACE, AFT CORNER IS BENT, SEPARATING, AND PULLED FASTENERS STA 1383. REPAIRED ON FASI WO 21117, NR12669.Jul 25, 2011 · N899AA · Boeing 727223 · Entrance StairsSDR FOTR2111712817Skin · debondedLT INBD FOREFLAP UPPER SURFACE HAS 6"DIAMETER DISBOND. REPAIRED ON FASI WO 21117, NR 12817.Jul 25, 2011 · N899AA · Boeing 727223 · Trailing Edge FlapsSDR FOTR2111712507Frame · dentedFWD CARGO COMPARTMENT- DENT AT STA 700 BETWEEN STR 23L AND 22L. REPAIRED ON FASI WO21117, NR 12507.Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2111712341Frame · dentedFWD CARGO COMPARTMENT-DENT AT STA 520 LT, STR 23L. REPAIRED ON FASI WO 21117, NR 12341.Jul 25, 2011 · N899AA · Boeing 727223 · Fuselage Main, FrameSDR C8GA2011000011Warning Horn · false activationDURING TAKEOFF ROLL, THE TAKEOFF WARNING SYS HORN SOUNDED. THE ACFT GROUND SPEED DID NOT EXCEED 20 KNOT. THE ACFT RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP AND OPS CHECKS WERE PERFORMED, NO DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Jul 13, 2011 · N898AA · Boeing 727223 · Independent InstrumentsSDR C8GA2011000008Flap System · lack of lubeDURING DEPARTURE, ON FLAP RETRACTION THE OTBD FLAPS WOULD NOT RETRACT ABOVE 4 DEGREES. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED, FLAP SYS WAS LUBRICATED AND OPS CHECK PERFORMED WITH NO DEFECTS NOTED. ACFT WJun 24, 2011 · N715AA · Boeing 727223 · Trailing Edge Flap Control SystemSDR C8GA2011000006Power Supply · inoperativeDURING TAKEOFF ROLL OUT, ALL 3 ENGINE FUEL FLOW INDICATIONS FLUXUATED BY + / - 5000 LBS. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING FUEL FLOW POWER SUPPLY AT FAULT. R & R THE FUEL FLOW POWJun 17, 2011 · N715AA · Boeing 727223 · Engine Fuel Indicating SystemSDR C8GA2011000004Engine · damagedON TAKEOFF DEPARTING, WHILE CLIMBING THROUGH 1000' A LOUD BANG EMERGED FROM THE NR1 ENGINE. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT NR 1 ENGINE REQUIRES REPLACEMEJun 10, 2011 · N715AA · Boeing 727223 · Engine (Turbine/Turboprop)SDR FY4Y20110315Splice · corrodedTHE EXFOLIATION CORROSION IS FOUND AT LT I/B MID FLAP CHORD SPLICE AT WBL 193 DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE CHORD SPLICE IS 0.072”. AFTER BLENT OUT, THE DIMENSION OF THE CORROSION AREA IS 3" (LENGTH) X 1 (WIDTH) AND REMAINDER THICKNESS IS 0.Mar 14, 2011 · N705AA · Boeing 727223 · Trailing Edge FlapsSDR FY4Y197M20110315ESeat Track · corrodedDURING PERFORMED CPCP CARD NR C53-224-01 PART 1 OF 3 FOR MAIN DECK CARGO COM'P FLOOR STRUCTURE, THE SEAT TRACK AT STA BS 640+3 AND BS 640+10 LBL. 0 WAS FOUND LEVEL 2 CORROSION. REPAIR METHOD IAW SRM 53-10-5 FOR FURTHER PROCESSING.Mar 11, 2011 · N705AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR FY4Y201103151Spar · corrodedTHE EXFOLIATION CORROSION IS FOUND AT LT INBD MID FLAP AFT SPAR LOWER CHORD AT WBL 82, DURING 6C CHECK. THE ORIGINAL THICKNESS OF THE CHORD IS 0.125". AFTER BLENT OUT, THE DIMENSION OF THE CORROSION AREA IS 3" (LENGTH) X 1" (WIDTH) AND REMAINDER THICKNESS ISMar 11, 2011 · N705AA · Boeing 727223 · Trailing Edge FlapsSDR FY4Y197M20110315DBeam · corrodedRT HORIZONTAL STAB TRAILING LOWER BEAM SURFACE STA 220 TO 222 HAD EXFOLIATION CORROSION. ORIGINAL THICKNESS IS 0.105". AFTER CORROSION REMOVED, THE REMAINED THICKNESS WAS 0.065", AREA WAS 2.75" X 1". IT'S BEYOND LIMITED IAW SRM 55-10-1, PAGE 1, NOTE B. CORROSMar 11, 2011 · N705AA · Boeing 727223 · Horizontal Stabilizer StructureSDR FY4Y197M20110315CBeam · corrodedLT HORIZONTAL STAB TRAILING LOWER BEAM UPPER SURFACE STA 66 TO 70 HAD EXFOLIATION CORROSION. ORIGINAL THICKNESS WAS 0.091". AFTER CORROSION REMOVED, THE REMAINED THICKNESS WAS 0.025", AREA WAS 4" X 1". IT'S BEYOND LIMITED IAW SRM 55-10-1, PAGE 1, NOTE B. CORMar 11, 2011 · N705AA · Boeing 727223 · Horizontal Stabilizer StructureSDR FY4Y197M20110310Skin Panel · corrodedDURING PERFORMED 6C-CHECK FOUND FUSELAGE EXTERIOR SKIN CORRODED (LEVEL 2) AT BS 1066 BETWEEN S-27L AND S-28L, IAW SRM 53-30-1, PAGE 2A PENETRATED DEPTH OUT OF LIMIT.Mar 7, 2011 · N705AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR FOTR2021700540Skin · corrodedCORROSION ON RT HORIZ STAB UPPER T/E SKIN AT NR 3 ELEVATOR HINGE CUTOUT. REMOVED CORROSION ON RT HORIZ STAB T/E BEAM WITH 100 PERCENT MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1 AND 55-10-1. FITTED NEW BEAM PN 65-24571-2, SN BN574 AND LOCATED HOLJan 26, 2011 · N708AA · Boeing 727223 · Horizontal Stabilizer, Plate/SkinSDR FOTR2021700137Hinge · crackedUPPER HINGE AFT MOST SEGMENT HAS AFT LOBE CRACKED. REMOVED AFT HINGE SEGMENT IAW SRM 51-30-2 AND 200F MM CH 52, FIG 5210B. FABRICATED NEW HINGE SEGMENT FROM MS20001-16-7200 PO 2021728 DIM 18" LONG. INSTALLED NEW HINGE SEGMENT IAW SRM 51-30-2 AND 51-10-2 AND Jan 26, 2011 · N708AA · Boeing 727223 · Fuselage, Door HingeSDR FOTR2021700257Angle · crackedRT WHEELWELL VERTICAL ANGLE IS CRACKED AT BS 870, RBL 8 BELOW LOAD CONTROL VALVE. REMOVED SUPPORT STRUCTURE AND VERTICAL ANGLE AT BS 870, RBL 8 FOR REPAIR IAW SRM 51-30-2. REPAIRED BS 870 WEB IAW SRM 53-10-9, FIG 5. FABRICATED 4 EA REPAIR FILLERS FROM 202Jan 26, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR2021700544Skin · corrodedCORROSION ON LT HORIZ STAB UPPER SKIN AT NR 4 ELEVATOR HINGE CUTOUT. REMOVED CORROSION ON LT HOR STAB T/E SKIN BEAM AT NR 4 HINGE CUTOUT. MEASURED .040" MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1, 51-10-6 AND 55-10-1. REMOVED LT HORIZ STAB T/E Jan 26, 2011 · N708AA · Boeing 727223 · Horizontal Stabilizer, Plate/SkinSDR FOTR2021700623Stringer · damagedSTA 540 AT STR 18R HAS HOLE DRILLED THRU RADIUS OF STRINGER. CUT OUT DAMAGED STRINGER DIM 19.5" LONG FROM STR 18R. FABRICATED NEW STRINGER SECTION FROM BAC1498-141 FROM 7075T6, PO 20041102, DIM 19.5", FABRICATED NEW TOP HAT FROM BAC1498-131, PO 90010803, DIMJan 26, 2011 · N708AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR FOTR2021700212Attach Bracket · crackedLT WING NR 2 SLAT ACTUATOR, INBD ATTACH BRACKET IS CRACKED. SLAT STA 291.0 REMOVED SLAT ACTUATOR SUPPORT STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STIFFENER FROM BAC1503-100145 PO NR 20217147 DIM 9" X 4.5" AND SHIM FROM 7075T6 .032" PO NR 9006027 DIM 5" X Jan 26, 2011 · N708AA · Boeing 727223 · Wing, Attach FittingsSDR FOTR2021700805Structure · damagedNR 3 PYLON DAMAGED. REMOVED TITANIUM DOUBLER FROM NR 3 PYLON IAW SRM 51-30-2 AND EA 2708-5401 REV 1, LOCATED AND DRILLED NEW TITANIUM DOUBLER PN 69-18227-2, PO 20217102 IAW SRM 51-30-5 AND 51-30-6. FABRICATED 2 EA, FREEZE PLUGS FROM 15-5PH .375 PO 20217121 DIJan 25, 2011 · N708AA · Boeing 727223 · Nacelle/Pylon, Main FrameSDR FOTR20217842Fitting · corrodedFUSELAGE EXTERIOR BS 740 PRESSURE FITTING IS CORRODED BETWEEN STR 27L-28L. REMOVED FITTING FROM STA 740 IAW SRM 51-30-2, FORMED FITTING FROM 7075-0, 7.2" X 10.7" .190" PO 2905745 IAW SRM 51-20-1, FIG 7. HEATED TREATED FITTING TO 7075T6 IAW ENG REPORT 2-37153-Jan 25, 2011 · N708AA · Boeing 727223 · Fuselage Main, Attach FittingsSDR FOTR/2021700365Fairing · gougedRT WING, OTBD FLAP, MID FLAP OTBD FAIRING HAS 2 EA GOUGES AND 1 EA LOOSE FASTENER. CUTOUT DAMAGED AREA DIM 1.5" X .6" IAW SRM 57-20-4, FIG 1. FABRICATED 2 EA REPAIR DOUBLERS FROM 2024-T3 .050" PO 90010715 DIM 5.6250" X 2.7500" AND 4.7" X 2". FABBED REPAIR Jan 25, 2011 · N708AA · Boeing 727223 · Trailing Edge FlapsSDR FOTR2021700828Frame · damaged(FOTR) MAIN CABIN FRAME AT BS 720A BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLE. CUTOUT DAMAGED AREA, DIMENSION 1" X .75" IAW SRM 51-10-1. FABRICATED DOUBLER FROM 7075-T6 PO 90010361, .063" DIMENSION 5.8750" X 3.8750" IAW SRM 51-40-3, FIG 1. INSTALLED REPAIR PJan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR/20217/00827Frame · damaged(FOTR) MAIN CABIN FRAME AT BS 700 BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLES. CUTOUT DAMAGED AREA AT BS 700 DIMENSION 1" X .8" IAW SRM 51-10-1. FABRICATED DOUBLER FROM 7075-T6 .063 PO 90010361, DIMENSION 6.8750" X 3.5" IAW SRM 51-40-3, FIG 1. INSTALLED REPAIJan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR/20217/00826Frame · damaged(FOTR) CABIN FRAME AT BS 680 BETWEEN STR 16L-17L HAS DOUBLE DRILLED HOLES. CUTOUT DAMAGED AREA DIMENSION 1.4" X .6" ON BS 680 BETWEEN STRINGER 16L-17L IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR ANGLE FROM 7075-T6 .050" PO 9009353 DIMENSION 7" X 3.6" IAW SRM Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2021700821Frame · dented(FOTR) CABIN FRAME AT BS 560 BETWEEN STR 15R-16R DENTED. CUTOUT DAMAGED AREA ON BS 560 BETWEEN STR 15R-16R, DIMENSION 1.1" X 1.1" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR ANGLE FROM 7075-T6 .071' PO 9009519, DIMENSION 6.5" X 3.5" AND REPAIR FILLER FROM 7075-Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2021700725Seat Track · corroded(FOTR) MAIN CABIN CARGO DECK, AT BS 560-580 LBL 45 INBD SIDE OF SEAT TRACK FLANGE HAS CORROSION. REMOVED CORROSION ON CABIN SEAT TRACK LBL 45, BS 560-580 IAW SRM 51-10-1, FOUND OUT OF LIMITS. REMOVED SEAT TRACK FROM BS 480-689 IAW SRM 51-30-2. FABRICATED SEAJan 11, 2011 · N708AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2021700682Seat Track · corroded(FOTR) LT FUSELAGE CABIN INTERIOR, HAS SURFACE CORROSION ON SEAT TRACK FLANGE BETWEEN BS 720A-720D, LBL 24. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FABRICATED NEW SEAT TRACK FROM BAC1520-792 7178-T6511 PO 90010776 DIMENSION 17'1.7500"Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR202170064Frame · dented(FOTR) LT FUSELAGE CABIN INTERIOR HAS FRAME DENTED AT BS 720, STR 16L. CUTOUT DAMAGED AREA ON FRAME DIMENSION 9" X .9" AT BS 720, STR 16L IAW SRM 51-10-1. FABRICATED FRAME REPAIR FROM 7075-T6 .063" PO 90010361, DIMENSION 5.5" X 17.3" IAW SRM 51-40-3, FIG 1. TJan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2021700661Frame · cracked(FOTR) REMOVED DAMAGED AREA FROM FRAME AT STR 17L DIMENSION 2.2500" X 1.5" IAW SRM 51-10-1, AND 51-30-2. FABRICATED REPAIR IAW SRM 51-40-3 FROM 7075-0 DIMENSION 9.1" X 4.1" PO 20198132. HEAT TREATED TO 7075T6 IAW FASI REPORT 2-37153-801A. FABRICATED CLIP FROJan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2021700658Stringer · gouged(FOTR) FUSELAGE CABIN INTERIOR HAS GOUGE AT FRAME BS 360 STR 6L. CUTOUT DAMAGED AREA AT STR 6L BS 360, DIMENSION 9.8750" FABRICATED STR FILLER FROM BAC 1498-143-7075T6 DIMENSION 9.8750". FABRICATED STRAP PLATES NR1 (1 EA) FROM 2024T3 .250" DIMENSION .8" X 1Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR FOTR2021700656Intercostal · cracked(FOTR)FUSELAGE CABIN INTERIOR, INTERCOSTAL IS CRACKED AT STR 16L BETWEEN BS 348-360. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR FROM 2024-T3 .063 PO 90010689, DIMENSION 5" X 3" IAW SRM 51-40-2. TREATED AND PRIMED IAW SRM 51-10Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR2021700653Shear Tie · cracked(FOTR) FUSELAGE CABIN INTERIOR, HAS CRACK INDICATION ON SHEARTIE, STR 8R BS 1130. REMOVED FASTENERS AT FUSELAGE FRAME IN MAIN CABIN BS 1130 STR 8R IAW SRM 51-30-2. C/W HFEC INSP IAW NDTM 51-00-00, FIG 23, PART 6. NO CRACKS NOTED. CUT SHEARTIE DIMENSION 6.2' X Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Internal Mounting StructureSDR FOTR2021700651Web · cracked(FOTR) CABIN INNER WEB DENTED AT BS 640, STR 6L. (AFT MAIN CARGO DOOR). C/W HFEC ON WEB IAW NDTM 51-00-00 FIGURE 23, PART 6. CRACK FOUND. REMOVED TRIM PANEL FROM BS 520-600, REMOVED AFT UPPER INNER SKIN FROM BS 600-560. FABRICATED NEW INNER SKIN FROM 2024-T3 .Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR2021700631Skin · dented(FOTR) AFT LOWER FUSELAGE EXTERIOR SKIN LT SIDE AT STATION 1148-1160 AND BETWEEN STR 25L-26L, SKIN IS DENTED. CUT DAMAGED AREA OUT OF UPPER LAP SKIN DIMENSION 4.5" X 5.5". FABRICATED REPAIR FILLER FROM 2024-T3 .063 PO 90010580 DIMENSION 12" X 14". FABRICATED Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR FOTR2021700626Stringer · corroded(FOTR) STR 27L BETWEEN BS 720F-740 IS CORRODED. CUT DAMAGED STR DIMENSION 12" LONG IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR STR FROM BAC1498-147 7075T62 PO 2014059 DIMENSION 11.4375" LONG AND FABRICATED REPAIR STR SPLICE FROM BAC1498-131 7075-T6 PO90010803 DIJan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR FOTR/20217/00507Intercostal · dented(FOTR) C1 DOOR CUTOUT INTERCOSTAL IS DENTED AT UPPER FLANGE BS 627 BETWEEN STR 24R-25R. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-30-2. LOCATED AND DRILLED NEW INTERCOSTAL PN 65-56101-36, PO 2021752. AND INSTALLED AT BS 627 BETWEEN STR 24R-25R IAW SRM 51-30-2,5Jan 11, 2011 · N708AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR/20217/00381Frame · dented(FOTR) CABIN FRAME DENTED AT BS 400 BETWEEN STRINGER 5R-6R. REMOVED DAMAGED AREA OF BS 400 FRAME AT STR 5R-6R DIMENSION 2.25" X 4" IAW SRM 53-10-4 FIG 1, FABRICATED REPAIR FILLER AND 2 EACH SPLICES FROM 7075-0, .050, PO 90010501 AND HEAT TREATED TO T-6 IAW SJan 11, 2011 · N708AA · Boeing 727223 · Fuselage Main, Frame
Back to Boeing 727-223