N70542

CESSNA L-19A · Fixed-wing single-engine · 1 engine · 2 seats · Valid Registration

Registered owner: KRECH GORDON L, ND (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

Accident · 1966-02-13 Unresolved
PIPER J-3 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case MKC66D0433

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

47 reports on file, 1995-09-02 – 1998-09-22.

OTHER · 1998-09-22 Matched by certificate designator
ATA 5753

Part: VANE — GOUGED (RT TE FLAP)

INSPECTION FOUND RT WING UPPER MOVEABLE VANE LEADING EDGE GOUGED. A REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 1, 51-10-4, 51-10-3, 51-30-2, AND 51-10-2.

Source: SDR CALA9801853
OTHER · 1998-09-19 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (BS 160)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 160, LONGERON 26R. THE DENTED AREA WAS CUT OUT IAW ECRA 5331-01030. DOUBLERS AND FILLER WERE INSTALLED IAW ECRA 5331-01030, SRM 51-10-3 AND 51-30-2.

Source: SDR CALA9801836
OTHER · 1998-09-17 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (BS 203.9)

INSPECTION FOUND FORWARD COCKPIT CO-PILOT'S SEAT TRACK CORRODED AT STA 203.9. THE SEAT TRACK WAS REMOVED AND REPLACED IAW MM 53-40-1.

Source: SDR CALA9801812
F.O.D. · 1998-09-17 Matched by certificate designator
ATA 5330

Part: SKIN — LIGHTNING STRIKE (BS 246)

INSPECTION FOUND LIGHTNING STRIKE DAMAGE IN LT FUSELAGE SKIN AT STRINGER 25L, STA 246. THE DAMAGED AREA WAS CUT OUT, DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5331-01031.

Source: SDR CALA9801813
OTHER · 1998-09-15 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (BS 259 & 265)

INSPECTION FOUND TOP OF FUSELAGE AFT ADF LOOP ANTENNA MOUNTING SURFACE EXTERNAL SKIN CRACKED AT RT CENTER MOUNT HOLE, STA 259 LONGERON 1R, BL 0 AND AT RT MOUNT HOLE, STA 265, LONGERON 1R, BL 0. BOTH CRACKS WERE .375 INCH LONG. THE CRACKED AREAS OF SKIN WERE CUT OUT. DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 29 AND 51-10-3.

Source: SDR CALA9801778
OTHER · 1998-09-14 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (BS 950)

INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 950, THREE INCHES BELOW LONGERON 14L. THE CRACKED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38.

Source: SDR CALA9801746
OTHER · 1998-09-14 Matched by certificate designator
ATA 5400

Part: WEB — CRACKED (NR 1 PYLON)

INSPECTION FOUND THREE 2 INCH CRACKS ON NR 1 ENGINE PYLON INTERNAL WEB AT STA 1065. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 54-01, FIGURE 2.

Source: SDR CALA9801748
OTHER · 1998-09-14 Matched by certificate designator
ATA 5510

Part: FAIRING — DELAMINATED (LT HORIZ STAB)

INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FAIRING DELAMINATED FROM AFT ATTACH POINT FORWARD. REMOVED PAN ON LOWER SURFACE AND REMOVED DELAMINATED HONEYCOMB. NEW HONEYCOMB WAS BONDED IN LOWER PAN AND THEN PAN WAS INSTALLED ON FAIRING AND BONDED IAW SRM 51-70-2 AND ECRA 5510-01316.

Source: SDR CALA9801752
OTHER · 1998-09-14 Matched by certificate designator
ATA 5311

Part: FRAME — GOUGED (BS 332)

INSPECTION FOUND FRAME GOUGED AT STA 332, LONGERON 29L TO 30. A SPLICE AND PLATE REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2A AND 51-10-2A.

Source: SDR CALA9801750
OTHER · 1998-09-14 Matched by certificate designator
ATA 5753

Part: FITTING — GOUGED (LT TE FLAP VANE)

INSPECTION FOUND FLAP FITTING GOUGED AT AFT END OF LT WING AFT MOVEABLE VANE INBOARD TRACK STA XFLS 65.612 TO 69.125. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Source: SDR CALA9801749
OTHER · 1998-09-14 Matched by certificate designator
ATA 5523

Part: TAB — DELAMINATED (LT ELEVATOR)

INSPECTION FOUND TWO AREAS OF DELAMINATION ON UPPER SURFACE OF LT ELEVATOR CONTROL TAB BETWEEN THIRD AND OUTBOARD HINGES. THE DELAMINATED AREAS WERE TRIMMED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-2.

Source: SDR CALA9801747
OTHER · 1998-09-14 Matched by certificate designator
ATA 5510

Part: FAIRING — DELAMINATED (RT HORIZ STAB)

INSPECTION FOUND RT LOWER HORIZONTAL STABILIZER FAIRING DELAMINATED AT FWD END. THE DELAMINATED HONEYCOMB CORE, DOUBLER, AND PLATE WERE REMOVED. BONDED DOUBLER WITH HONEYCOMB CORE AND PLATE TO SKIN FAIRING IAW ECRA 5510-01317, SRM 51-70-2, 51-30-2.

Source: SDR CALA9801751
OTHER · 1998-09-09 Matched by certificate designator
ATA 5320

Part: HAT CHANNEL — CRACKED (BS 756)

INSPECTION FOUND A 3 CRACK IN HAT CHANNEL AT FLOORBOARD PANEL, LT SIDE, STA 756. A NEW HAT CHANNEL SECTION WAS INSTALLED IAW SRM 53-05, PAGE 1 AND 51-30-2.

Source: SDR CALA9801685
OTHER · 1998-09-09 Matched by certificate designator
ATA 5320

Part: BRACKET — CORRODED (BS 917)

INSPECTION FOUND SUPPORT BRACKET CORRODED AT STA 917, STRINGER 28L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-3, 51-10-4, AND 51-30-1.

Source: SDR CALA9801686
OTHER · 1998-09-08 Matched by certificate designator
ATA 5510

Part: FAIRING — CRACKED (RT HORIZ STAB)

INSPECTION FOUND A 4.5 INCH CRACK IN LOWER AFT END OF RT HORIZONTAL STABILIZER LOWER FAIRING. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 55-11-0 FIGURE 7, 55-01, FIGURE 2, 51-10-3, AND 51-30-2.

Source: SDR CALA9801659
OTHER · 1998-09-08 Matched by certificate designator
ATA 5320

Part: DOUBLER — CRACKED (BS 945)

INSPECTION FOUND TWO 1 INCH CRACKS IN DOUBLER AT STA 945, LONGERON 14R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 28.

Source: SDR CALA9801654
OTHER · 1998-09-08 Matched by certificate designator
ATA 5321

Part: FLOOR — CRACKED (BS 756)

INSPECTION FOUND 1 INCH CRACKS AT CLIP NUT HOLES IN FLOOR PANEL NR 47 FORWAD OF STA 756. A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-21, 51-30-2, AND 53-05, FIGURE 1.

Source: SDR CALA9801653
OTHER · 1998-09-04 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 980)

INSPECTION FOUND A 1 INCH CRACK AT UPPER MOUNT HOLE OF FRAME AT STA 980, LONGERON 16R. THE CRACKED AREA WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-1.

Source: SDR CALA9801636
OTHER · 1998-09-02 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (BS 370)

INSPECTION FOUND WEB CORRODED AT FORWARD CARGO DOOR, STA 370, STRINGER 28R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.

Source: SDR CALA9801621
OTHER · 1998-09-02 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (BS 1062)

INSPECTION FOUND A .25 INCH CRACK AT FASTENER IN TAIL SECTION SKIN AT STA 1062 APPROXIMATELY FOUR INCHES BELOW LONGERON 15L. THE FASTENER WAS REMOVED IAW SRM 51-30-2 AND THE CRACKED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 28. A DOUBLER REPAIR WAS INSTALLED IAW 51-10-3.

Source: SDR CALA9801620
OTHER · 1998-09-02 Matched by certificate designator
ATA 5312

Part: BULKHEAD STRAP — CRACKED (BS 737)

INSPECTION FOUND A 1 INCH CRACK IN LOWER SUPPORT STRAP OF FORWARD BULKHEAD WALL IN AFT PIT, FS 737. THE SUPPORT STRAP WAS REMOVED AND A NEW SUPPORT STRAP WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.

Source: SDR CALA9801619
OTHER · 1998-09-01 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 965)

INSPECTION FOUND A 2 INCH CRACK IN LONGERON 17L AT ANGLE MOUNT, STA 965. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02, FIGURE 18. A NEW LONGERON SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-5.

Source: SDR CALA9801610
OTHER · 1998-08-28 Matched by certificate designator
ATA 5320

Part: CLIP — CRACKED (BS 965)

INSPECTION FOUND A 2 INCH CRACK IN SHEAR TIE CLIP AT LT AFT CABIN STA 965 UNDER LONGERON 13L. THE CRACK WAS REMOVED AND A CLIP REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 28.

Source: SDR CALA9801586
OTHER · 1998-08-28 Matched by certificate designator
ATA 5230

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR SKIN AT LOWER AFT CORNER. THE CRACKED AREA WAS CUT OUT AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 4.

Source: SDR CALA9801585
Earlier reports · 1995–1996 · 23 reports

1996

OTHER · 1996-08-09 Matched by certificate designator
ATA 5350

Part: CABLES — OUT OF ADJUST (TAILCONE)

TAILCONE RELEASE USING INTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-00.

Source: SDR CALA9601153
OTHER · 1996-08-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (BS 594)

INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 594, LONGERON 17R. THE CORROSION WAS REMOVED AND AN INTERNAL DOUBLER WAS INSTALLED IAW ECRA 5330-02427.

Source: SDR CALA9601194
OTHER · 1996-08-01 Matched by certificate designator
ATA 5522

Part: SKIN — CRACKED (RT ELEVATOR)

INSPECTION FOUND A 5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT STA XHS 86.0. AN EXTERNAL DOUBLER WAS INSTALLED IAW ECRA 5530-01174 AND SRM 55-03, FIGURE 13.

Source: SDR CALA9601195
OTHER · 1996-07-30 Matched by certificate designator
ATA 5521

Part: SPAR NUT — CRACKED (LT ELEVATOR)

INSPECTION FOUND, LT ELEVATOR MOST OUTBOARD BOTTOM NUT ON SPAR CRACKED. THE NUT WAS REMOVED AND REPLACED PER MM 20-16-0.

Source: SDR CALA9601114
OTHER · 1996-07-30 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 160)

INSPECTION FOUND LONGERON 3L CRACKED AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.

Source: SDR CALA9601192
OTHER · 1996-07-30 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 446)

INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5R. THE CRACKS WERE 2.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.

Source: SDR CALA9601224
OTHER · 1996-07-30 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 427)

INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5R. THE CRACKS WERE 1.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.

Source: SDR CALA9601223
OTHER · 1996-07-30 Matched by certificate designator
ATA 5511

Part: SPAR — CORRODED (LT HORIZ STAB)

INSPECTION FOUND CORROSION ON UPPER SPAR CAP OF LT HORIZONTAL STABILIZER FORWARD SIDE OF REAR SPAR AT STA XHS 95. THE CORRODED SECTION OF SPAR CAP WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 55-02, PAGES 85 TO 87.

Source: SDR CALA9601144
OTHER · 1996-07-30 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 427)

INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5L. THE CRACKS WERE 3.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.

Source: SDR CALA9601222
OTHER · 1996-07-30 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 200)

INSPECTION FOUND LONGERON 4L CRACKED AT STA 200. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2.

Source: SDR CALA9601191
OTHER · 1996-07-30 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 160)

INSPECTION FOUND LONGERON 4L CRACKED AT STA 160. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2.

Source: SDR CALA9601190
OTHER · 1996-07-30 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (BS 737)

INSPECTION FOUND LONGERON 5R CRACKED AT STA 737. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 2.

Source: SDR CALA9601198
OTHER · 1996-07-30 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 446)

INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5L. THE CRACKS WERE 3 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.

Source: SDR CALA9601225
OTHER · 1996-07-29 Matched by certificate designator
ATA 5312

Part: BULKHEAD ANGLE — CRACKED (BS 598)

INSPECTION FOUND A 3 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.

Source: SDR CALA9601226
OTHER · 1996-07-29 Matched by certificate designator
ATA 5312

Part: BULKHEAD ANGLE — CRACKED (BS 598)

INSPECTION FOUND A 1 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.

Source: SDR CALA9601227
OTHER · 1996-07-28 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 1143)

INSPECTION FOUND A CRACK IN FRAME JUST FORWARD OF RUDDER TRIM MOUNT AT TAIL COMPARTMENT STA 1143. A NEW ANGLE WAS INSTALLED ON FRAME IAW SRM 51-10-4.

Source: SDR CALA9601202
OTHER · 1996-07-28 Matched by certificate designator
ATA 5320

Part: SUPPORT — CRACKED (BS 484)

INSPECTION FOUND A .5 INCH CRACK ON FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 484, LONGERON 24R. A DOUBLER WAS INSTALLED IAW ECRA 5320C01263.

Source: SDR CALA9601193
OTHER · 1996-07-27 Matched by certificate designator
ATA 5230

Part: BEAM — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. A REPAIR WAS DONE IAW SRM 51-30-2.

Source: SDR CALA9601196
OTHER · 1996-07-27 Matched by certificate designator
ATA 5712

Part: RIB — CRACKED (NR 1 SLAT TRACK)

INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB AT NR 1 SLAT TRACK. THE RIB WAS REPAIRED IAW ECRA 5710-01751.

Source: SDR CALA9601201
OTHER · 1996-07-27 Matched by certificate designator
ATA 5230

Part: BEAM — CRACKED (CARGO DOOR)

INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT LOWER FORWARD STOP. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-3.

Source: SDR CALA9601200
OTHER · 1996-07-27 Matched by certificate designator
ATA 5230

Part: BEAM — CRACKED (CARGO DOOR)

INSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. THE BEAM WAS REMOVED AND REPLACED IAW SRM 52-01, FIGURE 1.

Source: SDR CALA9601197
OTHER · 1996-07-27 Matched by certificate designator
ATA 5230

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION FOUND A .375 INCH CRACK IN AFT CARGO COMPARTMENT DOOR FITTING INSIDE DOOR AT BOTTOM CENTER STOP. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Source: SDR CALA9601199

1995

FLUID LOSS · 1995-09-02 Matched by certificate designator
ATA 2820

Part: FUEL COUPLING — LEAKING (RT WING)

IAH - FLT 1230 - THE LEFT MAIN FUEL QUANTITY BEGAN TO DECREASE AS FUEL WAS TRANSFERRED FROM CENTER TANK AFTER TAKEOFF FROM IAH. THE LEFT FUEL QUANTITY STEADILY AND RAPIDLY DECREASED. THE CROSS-FEED WAS OPENED IN AN ATTEMPT TO BURN RT MAIN FUEL, BUT THE LT FUEL QUANTITY CONTINUED TO DECREASE. FUEL WAS REPORTED COMING FROM THE LT WING. THE CROSS-FEED WAS CLOSED AND THE ACFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RT WING INBD FUEL COUPLING LOOSE AND LEAKING FUEL. THE COUPLING PACKINGS WERE REPLACED AND THE COUPLING WAS RECONNECTED AND SAFTIED. LEAK CHECKS WERE GOOD. ALL FUEL BOOST PUMPS OPERATED NORMALLY AND NO LEAKS WERE NOTED. (X)

Source: SDR CAL950783